Canadian Aviation Service Difficulty Reports
Cessna 425 Corsair · Service Bulletins
Overview
This document is a quarterly publication by Transport Canada, focusing on Service Difficulty Reports (SDRs) that highlight issues affecting aircraft airworthiness in Canada. It compiles reports from various sources, including Aircraft Maintenance Engineers (AMEs) and operators, detailing defects, failures, and malfunctions that could pose safety hazards. The publication aims to inform the aviation community about these issues and promote awareness and corrective actions. Although it includes a variety of aircraft types, the Cessna 425 Corsair is specifically mentioned, making it relevant for operators and maintenance personnel of this model.
- Cessna 425 Corsair is mentioned in the context of Service Difficulty Reports.
- Operators must report all defects or occurrences to Transport Canada.
- Regular inspections and maintenance are critical to ensure airworthiness.
- Awareness of Airworthiness Directives (ADs) is essential for compliance.
- Unapproved parts can pose significant safety risks and should be avoided.
Document
Source
Originally published by tc.canada.ca. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Service Bulletins
- Year
- 2010
- Pages
- 42
- File size
- 4.6 MB
- Publisher
- tc.canada.ca
Common. Rarer than 24% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cessna 425 Corsair.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the CESSNA 425 Corsair to your watchlist and track it in one place.
More Cessna 425 Corsairmanuals & documents
- CAP 747 Mandatory Requirements for AirworthinessService Bulletins
- ANO (AW) Part 66- Aircraft Maintenance LicenceAirworthiness Directives
- Cessna Flyer - June 2015Pilot's Operating Handbook
- 2014 Notice of Names of Persons Appearing to be Owners of Abandoned and Unclaimed PropertyService Bulletins
- AOPA PILOT February 2013Checklist
- NOISE CONTOURS STUDY TORONTO CITY CENTRE AIRPORT Final ReportOther Documents
- Emergency Procedures for Cessna 425 CorsairEmergency Procedures
- Airworthiness Directive Schedule Aeroplanes Cessna 425Service Bulletins
- Pilot's Operating HandbookPilot's Operating Handbook
- B/CA Analysis: Cessna 425 CorsairPilot's Operating Handbook
- Prototype Airfield Capacity Spreadsheet Model User’s GuideChecklist
If you fly the Cessna 425 Corsair, you may also be researching these.
In this document
Hangar Noise
This section discusses the introduction of Canadian Airworthiness Regulation (CAR) 521, which supersedes previous standards. It highlights the changes in reporting suspected unapproved parts (SUP) and emphasizes the importance of reporting defects and malfunctions through the Service Difficulty Reporting Program.
Fixed Wing
The Fixed Wing section includes specific Service Difficulty Reports related to various aircraft, detailing incidents such as hydraulic failures and improper assembly of components. Each report provides insights into maintenance actions taken and recommendations for preventing similar issues.
Engines
This section covers engine-related Service Difficulty Reports, including incidents of overheating and missing components. It emphasizes the need for thorough inspections and maintenance practices to ensure engine reliability and safety.
Equipment Airworthiness Directives (ADs)
This section lists various Airworthiness Directives applicable to different aircraft, including the Cessna 425 Corsair. It provides details on the nature of each directive and the actions required by operators to maintain compliance.
FAA Unapproved Parts Notifications (UPNs)
This section outlines notifications regarding unapproved parts that could affect aircraft safety. It serves as a warning to operators and maintenance personnel to be vigilant about the parts used in their aircraft.
Safety notes
- Ensure correct orientation of parts before installation to avoid malfunctions.
- Inspect hydraulic lines and components regularly to prevent failures.
- Pay attention to the condition of flap cables to avoid asymmetrical flap conditions.
Full document text
Canadian Aviation Service Difficulty Reports Issue 2/2010 TC-1003961 TP 6980E (06/2010) TC-1003961 Feedback is published quarterly by the Continuing Airworthiness Division of Transport Canada, informing the aviation community of reported day-to-day problems that affect aircraft airworthiness in Canada. Reprints of original Feedback material are encouraged, but credit must be given to Transport Canada’s Feedback magazine. Please forward one copy of the reprinted article to the Editor. To obtain information concerning copyright ownership and restrictions on reproduction of the material, please address your correspondence to: Jérémie Laviolette, Editor Feedback Transport Canada (AARDG) Place de Ville, Tower C Ottawa ON K1A 0N8 E-mail: jeremie.laviolette@tc.gc.ca Tel.: 613-952-4360 Fax: 613-996-9178 Internet: www.tc.gc.ca/cawis-swimn The articles contained in Feedback are derived from Service Difficulty Reports (SDRs) submitted by Aircraft Maintenance Engineers (AMEs), owners, operators and other sources in accordance with Canadian Aviation Regulation (CAR) 521. SDRs are normally published verbatim. Transport Canada assumes no responsibility for the accuracy or content of any of these reports. Only spelling errors are corrected and content may be reduced as well as personal references are deleted. All defects or occurrences should be reported to Transport Canada through the Service Difficulty Reporting Program. For additional information about this program or concerning an article in Feedback magazine, contact your nearest Transport Canada Centre. Feedback est aussi disponible en français. © Her Majesty the Queen in Right of Canada, as represented by the Minister of Transport (2010). TP 6980E (02/2010) TC-1003961 TABLE OF CONTENTS Hangar Noise ........................................................................................................................................................... 3 Fixed Wing .............................................................................................................................................................. 3 Rotorcraft ............................................................................................................................................................... 10 Engines................................................................................................................................................................... 11 Heads Up (Feature Article) .................................................................................................................................... 12 Equipment Airworthiness Directives (ADs) .......................................................................................................... 13 FAA Unapproved Parts Notifications (UPNs) ....................................................................................................... 14 AME Symposium .................................................................................................................................................. 14 Suspected Unapproved Parts (SUPs) ...................................................................................................................... 15 FAA Special Airworthiness Information Bulletins (SAIBs) .................................................................................. 15 Service Difficulty Reports ...................................................................................................................................... 18 Civil Aviation Internet Sites: .................................................................................................................................. 42 Printed on Forest Stewardship Council compliant paper. To learn more, visit www.fsccanada.org Feedback 2/2010 3 HANgAr NOiSE Through Transport Canada’s initiative to harmonize with the Federal Aviation Administration (FAA) and Joint Aviation Authorities ( JAA), on 1 December 2009, Canadian Airworthiness Regulation (CAR) 521 came into force and superseded CAR standards 511, 513, 591 and 593. In order to better inform and familiarize the aviation community, Transport Canada would like to bring attention to the introduction of CAR 521 and specifically highlight a difference from the former CAR 591. Under the former CAR Standard 591, “Suspected Unapproved Parts” (SUP) were treated as an item within the SDR system. Now under CAR 521 this is no longer the case. SUP are now referenced in Standard 571.13 through an information note. The intent is that these suspected unapproved parts will still be reported using the tools available through the WSDRS program however they have a specific code to identify that they are not service difficulties. This change is also reflected on the SDR Logic Chart. The purpose of the SDR system is to collect, analyze, record and disseminate data concerning defects, failures and malfunctions which have resulted in, or may potentially, result in a safety hazard to an aircraft or its occupants. The SDR is still a mandatory report requirement and the purpose of the Web Service Difficulty Reporting System (WSDRS) procedure has not changed. Keeping the core function of the SDR process the same for all users. CAR 521 and its predecessor CAR 591 Service Difficulty Reporting F ixEd W iNg SWEARINGEN, SA226TC SDR # 20090918004 Ruptured Hose Causes Flapless Landing SDR submitted: Upon climb-out the aircraft's hydraulic warning lights illuminated and hydraulic pressure was lost. The aircraft returned to the airport and performed a flapless landing with the emergency gear handle activated. Maintenance discovered the hydraulic flexible hose from the hydraulic power pack to the accumulator in the L/H wheel well ruptured at a bend radius. The design of the aircraft required this hydraulic hose to have a significant bend in the hose so it could be routed correctly. Minor chaffing of the steel braiding on the hose was
Show full textShow less
found but was not significant enough to cause the rupture in the hose. The hose was replaced and the aircraft returned to service. 4 Feedback 2/2010 SWEARINGEN, SA226TC SDR # 20090106005 Bleed Air Control Valve - Improper Assembly SDR submitted: Maintenance replaced the bleed air valve solenoid after it was being reported as defective. Valve Part Number (P/N) 320250-4-1 is located in the R/H wheel well of the aircraft and by design is in fairly close proximity to the landing gear tires when the gear is retracted. After replacement of the valve, the AME did not notice the electrical connection for the valve was oriented differently than the valve previously removed. The wire harness and connector could be connected in this different configuration. Normally with the valve installed, looking forward the connector is at the 2 o’clock position. This replacement valve has the connector located at approximately the 6 o’clock position. The aircraft was dispatched and after takeoff, the crew retracted the gear and noticed the R/H main landing gear (MLG) remained in transit rather than locking in the up position. The gear was recycled with no success. The crew elected to return to the airport and landed without any further problems. Maintenance immediately noticed that the No. 3 tire had rub markings on it from contacting the bleed air valve solenoid’s connector during retraction attempts. This damaged the valve bracket and the cannon connector; the valve itself was not damaged. AMEs realigned the cannon plug connector and reinstalled the valve with a new bracket. They then, performed a gear swing and released the aircraft. The company has inspected the remaining valves in their fleet stock for any discrepancies that may cause this same occurrence. Transport Canada Comments: Ensure correct orientation of parts before installation. @ Incorrect Correct BEECh B200 SDR # 20090728011 Wing Rib Cracks (WS 121.966) SDR submitted: During inspection, the technician found cracked wing ribs at both the R/H and L/H wing rib leading edges located at Wing Station (WS) 121.966. The affected ribs were L/H wing ribs part numbers (P/N) 50-980002-825 & 000-11-133-21, and R/H wing ribs P/Ns 50-98002- 826 & 000-110133-22. The submitter stated that the cracks appeared to be caused from fatigue, as there was no evidence of a manufacturing tooling mark or other induced causes. It is of interest to note that three additional aircraft in the operator’s fleet also reported cracking of wing ribs. These cracks were all located at WS 121.966, which is immediately outboard of the engine nacelle. Transport Canada Comments: Engineering specialists opined that these wing rib cracks located at WS 121.966 were likely the result of vibrations coming from the propellers and engine mounts. A secondary factor may have been that landing loads were transferred to the subject wing ribs. In this case, the 3 aircrafts operate from gravel strips and have “approved STC” for larger tires and brakes installed. The Type Certificate Holder has been notified regarding this defect. @ Feedback 2/2010 5 SWEARINGEN, SA226TC SDR # 20090925005 Smoke in the Cockpit SDR submitted: On approach the crew had just selected full flap on the final landing checks when they noticed smoke in the cockpit. Since they were less than 5 km final, they elected not to put on their oxygen masks. The crew dumped cabin pressure, turned the bleed air off and turned the fresh air fan to override. Smoke continued to accumulate in the cockpit.The crew turned both generators off and continued on approach. After landing the crew informed Air Traffic Control that they had smoke in the cockpit, they immediately stopped the A/C and evacuated. Maintenance found that a flap down hydraulic line had ruptured at the L/H wing center section in the vicinity of the bleed air-mixing valve. The hydraulic fluid found its way into the air conditioning system and created the mist vapor event in the cockpit and cabin. There was no fire. The company replaced the line and cleaned the air conditioning system and released the aircraft. The company will be doing a fleet wide inspection to check for damaged hydraulic lines in these areas and ensure correct installation of the gaskets on the air conditioning valves. Transport Canada Comments: Although sometimes fretting is unavoidable, the need to inspect rigid lines and wires for chaffing cannot be stressed enough. @ GULFSTREAM - ISRAEL, GULFSTREAM 200 SDR # 20090715002 Windshield Terminal Arcing SDR submitted: While conducting the 1200 hour inspection of the R/H windshield, the “Anti Static Coating” on the G200 was found unserviceable and did not meet the specifications required in the manufacturer’s maintenance manual. The windshield required replacement and upon removal found that, one of the power cables arced to the aircraft’s structure due to poor insulation on the terminal end. The windshield and terminal end of the power cable were replaced. Transport Canada Comments: The operator ensured that the adequate clearance between the terminals and aircraft structure was obtained. @ 6 Feedback 2/2010 BEECh 1900C SDR # 20090619002 Flap Shaft Cable - Severed SDR submitted: During routine ground flap functional checks, the L/H outboard flap did not move, however the flap asymmetry switch activated as per design to prevent a split-flap condition. Upon further investigation, maintenance crew discovered that the L/H outboard flap cable was broken at the flap actuator end. The SDR submitter stated that corrosion was evident at the area of the cable breakage. It appears that if the flap outer cable sheath, is damaged or cracked, then pressurization air can force the lubricating grease out, thereby allowing moisture to enter the housing. This can result in binding and corrosion. Transport Canada Comments: A service history review revealed several previous flap cable failures where cable corrosion was evident in the flap drive sheathing and flap cable. The FAA issued AD 2001-18-07 (SB 27-3397) to inspect for any incorrectly configured flap flexible shaft assemblies that could result in an asymmetrical flap condition.Transport Canada recommends that owners/ operators pay frequent and particular attention to the condition of the flap cables. @ DhC 8 100 SERIES SDR # 20090604007 Main Landing Gear (MLG) – L/H Door Roller Seized SDR submitted: The sircraft landed with a L/H MLG indication snag. Maintenance crew put the aircraft on jacks and commenced troubleshooting. The first functional gear check was fine, however on the second selection, the L/H gear door did not open and the gear was “hanging up” on the door. The gear was then successfully selected back to the “up” position. However, when the Alternate (Emergency) Gear “down” selection was made, the gear still hung-up on the door, preventing full extension. Whenever the maintenance crew disconnected the door linkage, the landing gear extended as per normal. Further investigation revealed that the door roller for the L/H door was seized. This prevented normal door operation and subsequently prevented full gear extension. The SDR submitter stated that the forward door actuator and door roller is visually inspected at “A” check interval. The operator could not find any specific instructions for lubrication of the actual door roller. Transport Canada Comments: Bombardier have completed their investigation and determined that rigging related issues and damaged door linkages were the primary cause of this problem. @ Feedback 2/2010 7 BOMBARDIER, CL600 2D15 (705) 2D24 (RJ900) SDR # 20090624003/20090820010 Brake Line Quick Disconnect Fitting SDR submitted: After landing, the flight crew reported that the aircraft required a lot of power to taxi and the L/H side brakes seemed to be dragging. Once clear of the runway, they stopped on the taxiway and the tower confirmed that their No.1 Main Wheel was flat. Maintenance Personnel found the No.1 Main Wheel had a large flat spot and hole in it indicative of landing with a locked brake. The No.1 brake quick disconnect fitting was loose; it came off with only ½ turn. The loose fitting allowed hydraulic pressure to be trapped in the brake causing it to remain locked on landing. The quick disconnect fitting, product number H155006-191-001 (IPC 32-11-35, FIG. 1-180) was tightened and locked, both main wheels were replaced and the aircraft returned to service. The AME that completed this work mentioned that he has seen this issue before more then once, where the quick disconnect fitting is loose or in one case completely off (which caused the brake not to work at all). It appears that this fitting is susceptible to backing off if it is not correctly locked. Transport Canada Comments: The OEM is currently investigating this issue. In the interim, Transport Canada strongly recommends maintenance personnel to pay extra attention during maintenance activity around the wheels and brakes area. @ Fitting in the locked position Fitting is not locked On CRJ900 condition when hydraulic pressure is lost 3/4 of turn required FAIRChILD, SA227 AC SDR # 20090715001 Ignition Wiring Burns SDR submitted: During an engine start on the ground, it was noted that several circuit breakers popped at 10% engine speed when the auto ignition cut-in. After an in-depth inspection, wiring at the L/H wing lower fairing area was found burnt at multiple locations. The wiring was repaired and the aircraft returned to service. Transport Canada Comments: The operator is conducting a fleet inspection to determine if there are similar defects. @ 8 Feedback 2/2010 BOMBARDIER CL415 TURBO SDR # 20090129008 Cable Tension Compensator (Aileron/Rudder Interconnect) SDR submitted: During a routine inspection, the AME found the compensator assembly completely “jammed”. The operator then conducted similar inspections on all 8 remaining aircraft in their respective fleet. Several of the cable tension compensator assemblies were found seized and distorted (bent). Transport Canada Comments: On each aircraft both the cable compensator assemblies are installed on the fuselage roof between FS434.84 & FS481.50 Fuselage Stations. The interconnect between the rudder and aileron system is linked through a cam/ pulley, bellcrank and summing lever. The purpose of this assembly is to assist the pilot in making coordinated turns during flight operations. It is recommended that owners/operators closely inspect this assembly at the next opportunity. @ GULFSTREAM - ISRAEL, GULFSTREAM 200 SDR # 20090724004 L/H Engine Fire Loop Failure SDR submitted: On climb out at approximately 18 000 feet, the pilots reported that the L/H engine fire detection system indicated failed. The pilots reported that the checklist had been completed and as a precautionary measure proceeded to shut down the engine in flight. The aircraft was re-routed and declared an emergency. The tower reported that no flame or smoke could be seen from the L/H engine. After an uneventful landing, maintenance was called to investigate and found the Fire Loop in Zone 2 had failed. Gulfstream and Pratt & Whitney were informed of the failure. Further investigations revealed that the cause of the failure was a missed and unused clamp at the end of the loop. The Zone 2 Fire Loop was replaced, utilizing this last clamp a ¼ inch from the end of the loop, limiting frequency vibration. The aircraft was ground run and a functional check was carried out on the Fire Loop and all systems operated serviceable. Feedback 2/2010 9 DIAMOND DA42 SERIES SDR # 20090122002 Nose Landing Gear (NLG) Tubular Pivot Assembly SDR submitted: Several recent SDRs have described a misalignment problem regarding the NLG gudgeon (D60-3233-82- 31) within the tubular pivot shaft (D60-3233-82-32). The SDR submitter stated that the misalignment only occurs on the L/H gudgeon and always opens toward the aft direction; when the nose gear is down and locked. Another SDR reported the NLG failed due to shearing of the L/H gudgeon within the tubular shaft. As a result, the L/H wall of the wheel well was damaged directly due to NLG component mislocation. The NLG spring assembly and the NLG actuator driving the down lock mechanism can create excessive forces that the tubular pivot assembly cannot tolerate. Repeated forces on the gudgeon may result in a “belling” deformation on the tubular pivot shaft. Transport Canada Comments: Diamond Aircraft (Austria) has taken corrective action and recently issued Mandatory Service Bulletin (MSB) 42-070/1. The subject MSB provides instructions to check for excessive wear and gap between the Tubular Pivot and L/H Gudgeon. If the gap exceeds specified limits, the tubular pivot tube assembly will require replacement. Transport Canada (TC) strongly recommends that owners/operators comply with the aforementioned MSB. Failure to do so could possibly result in the collapse of the NLG. @ PILATUS - SW, PC 12 47E SDR # 20090805001 Passenger Door Shoot Bolt Unsafe SDR submitted: After a flight, the crew attempted and was unable to open the passenger door. The crew noted that the upper forward shoot pin indicator remained "green" with the handle in the open position. The door panel was removed for inspection and maintenance noted that the retaining bolt for the upper forward shoot pin had migrated out of position. The nut for the retaining bolt was found dislodged and had fallen within the door. The bolt and nut were reinstalled into the shoot pin linkage, the nut was torqued in safety and the aircraft was returned to service. Transport Canada Comments: The operator noted that no maintenance had been performed in this area since the manufacture of the aircraft and suspected that the nut was never torqued in safety during its initial installation. @ 10 Feedback 2/2010 rOTOrCrAFT AEROSPATIALE, AS 350B2 SDR # 20080722005 Main Rotor Head Ring Cracked SDR submitted: On a routine mast reconditioning and inspection, which have a 6-year inspection requirement, the ring was sent for non-destructive testing (NDT) along with the rest of the parts from the assembly (no NDT requirement for the ring at any point, or for any part of the assembly at the 6 year inspection). There was a stress crack during the Magnetic Particle Inspection (MPI) check, which was cause for rejection of the part. The ring is located at the top of the main rotor shaft, where the rotor head attaches, and rotates with the main rotor shaft/head. The customer was notified of the defect, and the part was replaced. Transport Canada Comments: A heads up to operators that this inspection should be implemented in their maintenance program. @ BELL TEXTRON - CANADA, 206B SDR # 20081125005 Vertical Fin Washers Cracked SDR submitted: The vertical fin was removed to facilitate seal replacement of the pitch change mechanism. The radius washers that are used on the vertical fin attachment were inspected, and it was noted that 3 of the 4 washers had cracks on the outside perimeter of the washer. The washers, part number 140-019-1, were replaced and the fin re-installed. Transport Canada Comments: It is not known if this condition is due to over tightening of the fastener, or the increase in torque value following issuance of Alert Service Bulletin 206-06-107. @ Feedback 2/2010 11 SIKORSKY, S76A SDR # 20090901001 Pitch Change Horn Cracked SDR submitted: A routine inspection revealed an apparent crack in the tail rotor pitch change beam. After removal of the protective paint coating, the existence of a crack was confirmed both visually and by the Liquid-Phase Infiltration (LPI) method. The crack extended from the outside diameter of the bushing outward to the outer edge of the horn. Due to the critical location of the discovered crack, the pitch change beam was replaced and the aircraft was returned to service. Transport Canada Comments: The operator added that they will implement a one-time inspection and have increased the inspection guidelines for repetitive inspection. @ ENgiNES GENERAL ELECTRIC, CF34-3B1 SDR # 20090728005 CF34-3B Missing Nut Engine bleed air port SDR submitted: Pilots reported L/H engine jet pipe overheat warning was activated during cruise for approximately 20 seconds and then went away by itself. Aircraft was returned to base. Maintenance investigated and found a plug/plate at approximately 11 o’clock with 1 nut loose and the other missing. The nut was found in the bottom of the cowl and the other nut was loose about 4 turns. Note: This plug is located at the same engine station as the Inlet Turbine Temperature (ITT) Probes. It is unclear whether hot gases were escaping from the loose plate and caused the jet pipe overheat warning or if the nut falling down and contacting the terminal lugs of the sense elements set off the warning. No reoccurrence of this fault has occurred since the reinstallation of the plug/plate. Transport Canada Comments: Good area to inspect at the next opportunity of engine maintenance activity.@ Bleed air cover, loose and missing nut IPC 72-51-00 Fig 1, Item 80 Top view, port located at 11 o’clock position Aft of engine 12 Feedback 2/2010 A recent SDR was issued where: “shortly after takeoff, the flight crew reported that abnormal control inputs and trim were required during climb-out and landing with flaps extended”. Initial maintenance inspections of both the flap and aileron systems revealed nothing out of the ordinary even though a complete operational and visual inspection was performed. A flight test was conducted and it was observed that the left out-board mid flap panel was not correctly aligned in relation to its adjoining flap panel and wing. Further maintenance investigations revealed that on the left wing out-board mid-flap, the in-board carriage spindle (number 2) had sheared. Another similar event had previously occurred where the aircraft was reported to roll to the right with flaps beyond 10 degrees and 15 units of trim was required to hold level flight. Once again the initial inspection revealed no obvious fault but a further investigation found the right wing out- board mid-flap in-board carriage spindle (number 7) had sheared. Back in July 2002, Boeing issued Alert Service Bulletin 737-57A1277 to address this issue due to a high number of spindle reported failures from several operators. Later that year in October, the Federal Aviation Authorities (FAA) issued AD 2002-22-05, which mandated a repetitive inspection interval task of all flap carriage spindles including a corrective action procedure. The following year FAA AD 2003-24-08 was issued, superseding the previous one, due to an operator that experienced a right wing mid flap dual carriage spindle failure (number 7 and 8) during approach. This event was defined as follows: “at approximately 500 feet above ground, the flight crew heard a loud bang followed by the aircraft rolling off hard to the right where significant aileron and rudder inputs were required to maintain level flight to complete the landing”. This new AD reduced the inspection interval and revised the overhaul procedure. For these events above and in all other cases that have been reported, the aircrafts controllability was affected, abnormal control inputs and trim were required by the flight crew to maintain normal level flight. As stated by an operator who experienced this scenario “the flap is very heavy and difficult to move, when trying to trouble-shoot for this type of failure”, emphasizes the importance to recognize this type of fault and to be aware of the Boeing 737 Maintenance Manual procedure 05-51-191 when trouble-shooting this type of snag. Due to the continuation of flap carriage failure incidents, Transport Canada Civil Aviation (TCCA) along with the FAA are presently reviewing all SDRs issued since the release of AD 2003-24-08. HEAdS Up (FEATUrE ArTiCLE) BOEING 737-100, -200, -200C, -300, -400 AND –500 SERIES SDR # 20100104005 Aircraft controllability and excessive trim Mid-flap carriage arm Carriage arm spindle Feedback 2/2010 13 EqUipmENT AirWOrTHiNESS dirECTivES (AdS) Transport Canada (TC) endeavours to send copies of new airworthiness directives (ADs), which are applicable in Canada to the registered owners of the affected products. Equipment/appliance ADs are often only distributed to our regional offices because the owners of aircraft affected by this type of AD are not generally known. AMEs and operators of the affected products are encouraged to obtain further information or a copy of the ADs from their regional TC office, their local TCC, their PMI, or from the Civil Aviation AD website at: www.tc.gc.ca/cawis-swimn Manufacturer AD Number Origin Description ROCKWELL COLLINS 2010-0067 EU ATA 34 - Navigation - Mode S Transponder - Check / Modification KELLY AEROSPACE 7/8/2010 US Rebuilt turbochargers FIRE FIGHTING 2010-0062 EU ATA 26 - Fire Protection – Halon 1211 Fire Extinguishers – Identification / Replacement HONEYWELL 7/2/2010 US To ensure that the flightcrew has an accurate glideslope deviation indication FIRE FIGHTING 2009-0262R1 EU Fire Protection - Halon 1211 Fire Extinguishers - Identification / Replacement RMH DEVELOPMENT 2/7/2010 US Main Rotor Blade failure. - Inspection LIFESAVING SYSTEMS 3/2/2010 US Replacement of Lifesaving Systems Corp. D-Lok Hook assembly FALLSCHIRMBAUBUCHSEN 2010-0009-E EU ATA 25 - Equipment / Furnishings - Emergency Parachute - Inspection / Rework ENGINE COMPONENT INC 2009-26-12 US Cracks at the head-to-barrel interface in the cylinder assemblies SICLI 2009-0278 EU ATA 26 - Fire Protection – Portable Halon 1211 Fire Extinguishers – Identification / Replacement ALLIED SIGNAL CF-2009-44 CF Emergency Locator Transmitter – Potential Failure To Transmit The Required 406MHz Coded Signal HONEYWELL CF-2009-44 CF Emergency Locator Transmitter – Potential Failure To Transmit The Required 406MHz Coded Signal B/E AEROSPACE 2009-21-10 US Rupture of a high-pressure gaseous oxygen cylinder, which had insufficient strength characteristics due to improper heat treatment - Replacement HAMILTON SUNDSTRAND 2009-21-03 US Over-fueling of the APU during the start sequence GOODRICH 2009-20-11 US ATA 28 - potential of ignition sources inside fuel tanks. ROCKWELL COLLINS 2009-0173 EU ATA 34 - Navigation – Mode S Transponder – Modification / Replacement. HARTZELL 10/14/2009 US Separation of the propeller blade counterweight slug FREEFLIGHT SYSTEMS 5/8/2009 US Erroneous information provided by 2101 I/O Approach Plus GPS navigation system. TRIMBLE 5/8/2009 US Erroneous information provided by 2101 I/O Approach Plus GPS navigation system. AVIDYNE 5/5/2009 US Primary Flight Display (PFD) altitude and airspeed information BENDIX 2/3/2009 US Fuel injection servo, having a servo plug gasket, part number (P/N) 365533. PRECISION AIRMOTIVE 2/3/2009 US Fuel injection servo, having a servo plug gasket, part number (P/N) 365533. 14 Feedback 2/2010 FAA UNApprOvEd pArTS NOTiFiCATiONS (UpNS) Unapproved Parts Notifications are published by: FAA, AIR-140, P.O. Box 26460, Oklahoma City, OK 73125. For a full list please visit: http://www.faa.gov/avr/sups/upn.cfm UNApprOvEd pArTS NOTiFiCATiONS NUmBEr SUBjECT dATE pOSTEd 2010-20090528001 MacLean - ESNA, Pocahontas, Arkansas - Non-conforming Locking Nuts 03/23/2010 2010-20090623001 Electrocube, Pomona, CA - Sold Transformer Power, Fixed Autotransformer without Parts Manufacturer Approval 02/17/2010 2010-20090909001 Non-conforming Thrust Reverser Actuator Clevis Pins for General Electric CF6-80C2 and CF6-80E1 Engines 01/12/2010 2010-20080616008 Isolair, Troutdale, OR - Selling UH-1H parts without approval 01/11/2010 2009-20090817004 Hoover Precision Products, Inc. - Bearing assemblies with improperly heat treated ball bearings 12/10/2009 2009-20090512001 Weatherly Aircraft Nevada, Bogalusa, LA - Selling aircraft parts without FAA approval 09/18/2009 2009-20080703001 Watson’s Profiling Corporation - Manufacturing Aircraft Parts without FAA Approval 09/9/2009 2007-00016 Elliptical Systems Incorporated Current Limiters, Overhead Reading Light Switches and Avia-Dynamics Corp. Coffee Brew Trays - Sold without Parts Manufacturer Approval 08/27/2009 2009-20080716034 Plymouth Tube Company-Failed to conduct all required testing as stated on Certificate of Compliance for stainless/ nickel alloy tube material supplied to Aerospace Industry 08/27/2009 2009-200600012 Chatsworth Rubber - Nonconforming MS and NAS O-Rings 08/17/2009 2009-200700141 Acme Components Company SMLJ15CD TR-T Diodes - Produced without Parts Manufacturer Approval 08/17/2009 AmE S ympOSiUm Ontario Ontario October 27-29, 2010 Delta Meadowvale Conference Centre 6750 Mississauga Rd Toronto, ON L5N 2L3 Tel: 905-405-1870 Fax: 905-405-1855 Email: cara@precisionaerocomponents.com Feedback 2/2010 15 SUSpECTEd UNApprOvEd pArTS (SUpS) The submitters of the following Service Difficulty Reports (SDRs), indicated that an unapproved part was suspected. The list is provided here for information only and should not be constructed as an identification of confirmed unapproved parts. In Canada, SUPs should be reported in accordance with Canadian Aviation Regulation (CAR) 521, indicating your suspicion of an unapproved part on a regular SDR form or on the Internet at www.tc.gc.ca/wsdrs Make/Model JASC Part Name Part No Part Condition SDR No. RGN Boeing 737 275 2000 HYD ACCUMULATOR 2660472M2 NEW 20091002004 PNR CeSSnA 172N 2000 WING FAIRINGS A221ANDA222 NEW 20090730002 ONT DeHAViLLAnD - CAn C6US100015 2000 AXLE ASSY C6US100015 NEW 20090701001 PNR DHC2C2UT473 2000 TORQUE TUBE C2UT473 CORRODED 20090817003 PAC DiAmonD - CAn 202720130 2000 RUDDER CABLES 2027201300 NEW 20091127006 PAC grimeS mFg Co 209075325 2000 FILTER PR 25026011 NEW 20090430005 PAC HoneyweLL JG7039C1 2000 CLAMP O316S INCORRECT ASSY 20091125006 PNR mCCAuLey C5013WPL 2000 SPRINGS INCORRECT PART 20090730006 PAC prAtt & wHitney - CAn 90478401A 2000 EXCITER LOOSE 20091007005 PNR teLeDyne BenDix 101630509 2000 HOUSING BROKEN 20091119006 PAC A Special Airworthiness Information Bulletin (SAIB) is an information tool that alerts, educates, and makes recommendations to the general aviation community. It is non-regulatory information and guidance that does not meet the criteria for an Airworthiness Directive (AD). http://www.faa.gov/aircraft/safety/alerts/SAIB/ SAiB NUmBEr mAkE / COmpANy SUBjECT iSSUE dATE NE-10-27 Superior Air Parts, Inc. Reciprocating Engine Oil System 04/20/2010 CE-10-26 Schempp-Hirth Flugzeugbau Engine – Starter Ring Gears 04/14/2010 CE-10-25 TKS Flammable Fluid Considerations for TKS Fluid 04/5/2010 NM-10-23 All-cargo Equipment/Furnishings: Exterior Exit Markings 03/31/2010 NM-10-24 Boeing Company, The Hydraulic Motors: Hydraulic Motor Generator (HMG) Inadvertent Lock-out 03/31/2010 CE-10-22 Honeywell Navigation 03/26/2010 CE-10-19R1 General Aviation Engine Exhaust and Carbon Monoxide Detectors 03/17/2010 CE-10-21 Propellers Propellers/Propulsers; Propeller Overspeed in Piston Engine Aircraft 03/17/2010 CE-10-20 Cessna Aircraft Company Wing Structure; Wingtip Extensions 03/16/2010 FAA S pECiAL AirWOrTHiNESS iNFOrmATiON BULLETiNS (SAiBS) 16 Feedback 2/2010 SAiB NUmBEr mAkE / COmpANy SUBjECT iSSUE dATE NM-10-18 ATR – GIE Avions de Transport Régional Instruments: Redesigned Aileron Sensors for Flight Data Recorder 03/4/2010 CE-10-17 Piper Aircraft, Inc. Landing Gear - Piper PA-28 and PA-32 Main Landing Gear Torque Link Inspection Interval 02/23/2010 CE-10-16 Liberty Aerospace Incorporated Passenger/Crew Doors: Liberty Aerospace Inc. XL-2 02/9/2010 SW-10-15 Bell Helicopter Textron (Canada) Bell Helicopter Textron, Inc. (Bell) Model 429 Helicopters with Clam Shell Doors 02/5/2010 CE-10-14 Honeywell/Bendix King Navigation 01/22/2010 SW-08-03R2 Rotorcraft Recommendations for Rotorcraft During Icing Conditions 01/15/2010 CE-10-11R1 General Aviation Electrical: Fire Hazard in Resetting Circuit Breakers (C/Bs) 01/14/2010 NM-10-12 Agusta S.p.A Cessna Aircraft Company Gulfstream Aerospace Corporation Hawker Beechcraft Corporation Honeywell. Navigation: Flight Management System 01/7/2010 NM-10-13 ATR – GIE Avions de Transport Régional Boeing Company, The Bombardier Inc Cessna Aircraft Company Dassault Aviation Embraer - Empresa Brasileira de Aeronautica S.A Gulfstream Aerospace Corporation Hawker Beechcraft Corporation Lockheed Martin Corporation Honeywell Navigation: Flight Management System 01/7/2010 CE-10-10 Hawker Beechcraft Corporation Controls: Flap Control System Rigging and Flap Actuator Overhaul 11/30/2009 NE-10-09 Rolls-Royce Motors, Ltd TeledyneContinental Motors Reciprocating Engine Power Section: Hydraulic Valve Lifters 11/20/2009 CE-10-08 Zodiac Wings: Zodiac CH601XL and CH650 Wing Structural Modifications 11/7/2009 NE-10-07 Teledyne Continental Motors Reciprocating Engine Cylinder: Identification Information for Superior Air Parts, PMA Cylinder Heads for Teledyne Continental Motors (TCM) IO-520, TSIO-520,and IO- 550 Series Engines. 11/2/2009 NE-09-51R1 Avia Propeller Ltd. Propeller Blade Section 10/29/2009 CE-09-37R1 True Flight Holdings LLC Stabilizer: True Flight (Grumman American) AA-5 10/23/2009 NM-10-06 Bombardier Inc. Oxygen—Inspection of Third Crewmember Oxygen Hose 10/20/2009 CE-09-40R1 CPAC, Inc.Gulfstream Aerospace Corporation Flight Controls - Trailing Edge Flap Control System 10/19/2009 NE-10-05 Reciprocating Aircraft Engines Fuel Control/Reciprocating Engines – Float type Carburetors 10/16/2009 CE-10-04 General Aviation Smoke Detection: Cockpit Smoke and Fumes 10/8/2009 CE-10-02 Glaser-Dirks Flugzeugbau GmbH Flight Controls: Aileron Control Rod End 10/7/2009 CE-10-03 Glaser-Dirks Flugzeugbau GmbH Flight Controls: Elevator Control Bearing Stand 10-07-2009 CE-10-01 Cessna Aircraft Company Fuel Tanks Fuel: Fuel Tank Selector Valve Systems 10-05-2009 Feedback 2/2010 17 SAiB NUmBEr mAkE / COmpANy SUBjECT iSSUE dATE CE-09-50 Cessna Aircraft Company Alternative Method of Compliance for AD 2008-15-06 09/23/2009 NE-05-84R1 Bombardier-Rotax GmbH Reciprocating Engine Liquid Cooling: Bombardier-Rotax 912 & 914 Series Engines 09/10/2009 SW-09-49 Eurocopter France Eurocopter AS350BA Emergency Floats 09/1/2009 NE-09-25R1 Fuel Fuel: Jet Fuel Containing FAME (Fatty Acid Methyl Ester) 08/19/2009 NE-09-48 Propellers 6110 Propeller Assembly 08/14/2009 CE-09-47 Flight Deck Navigation: VOR or LOC/ILS Approaches with G1000, Perspective™, Prodigy™ Integrated Flight Decks Installed With a Garmin GFC 700 Autopilot 08/7/2009 CE-09-46 Cirrus Design Corporation Landing Gear, Nose 07/31/2009 CE-09-45 Viking Air Limited Leveling & Weighing: Viking Air Limited DHC-2 MKI Gross Weight Increase Modification (STC SA00299NY) 07/29/2009 SW-09-44 Schweizer Aircraft Corporation Cabin door 07/28/2009 CE-09-42 Cessna Aircraft Company Lights - Landing Light, Beacon Light and Taxi Light Switch Applications 07/24/2009 CE-09-43 DaimlerChrysler Aerospace AG Alternative Method of Compliance for AD 87-09-01 07/24/2009 CE-09-41 Hawker Beechcraft Corporation Aft Baggage/Maintenance Door Latches 07/22/2009 NE-06-31R3 Lycoming EnginesTextron LycomingAVCO Corporation Engine Lubricating Oils 07/22/2009 NE-09-31R1 Textron Lycoming, AVCO Corporation, Turbochargers Turbocharging: Rebuilt by Kelly Aerospace Energy Systems 07/9/2009 CE-09-38 Mooney Aircraft Corporation Wings: Installation of Supplemental Type Certificate (STC) Wing Tip Fairings 07/7/2009 CE-09-39 Cessna Aircraft Company Leveling and Weighing: Maximum landing gross weight limitation for Cessna U206F, U206G, TU206F, TU206G series airplanes equipped with Flint Aero STC SA4366WE 07/7/2009 18 Feedback 2/2010 SErviCE diFFiCULTy rEpOrTS Make/ Model JASC Part Name Part No Part Condition SDR No. RGN AIRCRAFT Aero CommAnDer 112TCA 3220 BOLT AN415 SHEARED 20091117003 ONT 680F 5711 RIVETS AN4265 CORRODED 20090819007 PNR 680FL(P) 2910 HYDRAULIC TUBE RUPTURED 20091020006 PAC 681 2731 TRANSMITTER EA1502C1 FAILED 20091023003 PNR 690 3220 LANDING GEAR IN SERVICE 20090824003 PAC 690A 3200 PSI GAUGE 13551000509 OVERHAULED 20090623006 PNR 690A 5610 WINDOW LOOSE 20090625003 PNR 695A 2100 PRESSURIZATION LINE 8505345 BENT 20090922004 PNR AeroSpAtiALe AS 350B1 2931 HYDRAULIC PRESSURE SWITCH MA12401 INOPERATIVE 20091021015 PAC AS 350B1 2932 PRESSURE SWITCH MA12402 NEW 20090813010 PAC AS 350B2 0 PILOT SEAT BELT ASSY 504305401 SERVICEABLE 20090915009 PAC AS 350B2 2431 BATTERY 16061 OVERHEATED 20090810002 PAC AS 350B2 2435 SHAFT 150SG11032 SHEARED 20090820002 QUE AS 350B2 2900 HYDRAULIC HOSE ASSY 704A34412037 BURST 20090813015 PAC AS 350B2 2900 SWITCH MS2771923 UNSERVICEABLE 20091201002 ONT AS 350B2 2915 SWITCH MA12401 INOPERATIVE 20090723011 PAC AS 350B2 2932 HYDR PRESSURE SWITCH MA12401 INOPERATIVE 20090730010 PAC AS 350B2 3340 SWITCH 045004B110A UNSERVICEABLE 20090806002 ONT AS 350B2 5301 MANUAL RELEASE CABLE AS221826802 INCORRECT PART 20090423005 PAC AS 350B2 5347 LEAF 350A2113832403 CRACKED 20090526006 PNR AS 350B2 5450 ANGLE BRACKET 350A21126220 CRACKED 20090825004 PNR AS 350B2 5610 L/H WINDOW SLIDER 704A41512003 VIBRATING 20091215002 PAC AS 350B2 6420 T/R PITCH LINK 350A33214501 CRACKED 20090703002 PAC AS 350B2 6500 FLEX COUPLING 350A35105901 CRACKED 20090716009 PAC AS 350B2 6730 ACCUMULATOR 704A34240015 FAILED 20090820003 QUE AS 350B2 6730 ACCUMULATOR 704A34240015 FAILED 20090820004 QUE AS 350B2 6730 ACCUMULATOR 704A34240015 FAILED 20090820005 QUE AS 350B2 7314 FUEL PUMP 430137702 LEAK 20090401014 ONT AS 350B3 3340 MOUNTING ADAPTER BRACKET LIP WORN 20090622013 ONT AS 350B3 6220 STATIC STOP YOKE ASSY 350A37116200 UNSERVICEABLE 20090420002 PNR AS 350B3 6320 NUT DHS43911142 LOOSE 20090703003 ATL AS 350BA 2822 FUEL BOOST PUMP P94B12209 FAULTY 20090910006 QUE AS 350BA 2913 HYDRAULIC PUMP 704A34310006 UNSERVICEABLE 20090413003 ONT AS 350BA 5302 DOUBLER OR PLATE 350A09014920 CRACKED 20090827007 PNR AS 350BA 6730 ACCUMULATOR 704A34240015 FAILED 20090820006 QUE AS 350BA 7300 FUEL CONTROL UNIT 164548540 FAULTY 20090715005 PNR AS 350BA 7921 OIL COOLER BLOWER MOTOR 9696 SHORTED 20090708004 PNR AS 355F2 6200 ROTOR INCORRECT PART 20090527002 ONT AS 355NP 2400 WIRING OF CAROUSEL SWITCH 83450001 NEW 20090702004 PNR ATR 42 300 2100 AIR CONDITIONING UNSERVICEABLE 20090807008 PNR ATR 42 300 2422 INVERTER FAULTY 20090824001 ONT ATR 42 300 2710 SENSOR AILERON POSTION 4820208 BROKEN 20091023001 PNR ATR 42 300 2923 PUMP POPPING 20090807007 PNR ATR 42 300 3210 WEIGHT ON WHEEL SWITCH D228780001 UNSERVICEABLE 20091005004 ONT ATR 42 300 3230 PROXIMITY SWITCH D22878001 DENTED 20090618007 ONT ATR 42 300 3260 LG WARNING CONTAMINATED 20090416005 ONT ATR 42 300 3422 EHSI 7003110912 UNSERVICEABLE 20091124003 ONT ATR 42 300 5210 DIAPHRAM S53G71268180 CRACKED 20090423011 ONT ATR 42 300 5610 WINDOW NP1588032 CRACKED 20090929005 ONT ATR 42 300 5610 WINDOW DISCREPANT 20090721002 PNR JASC: Joint Aircraft System Code number defining assembly/system/components SDR No.: Transport Canada Civil Aviation (TCCA) -assigned SDR control number — please quote in any correspondence or inquiries RGN: TCCA region of SDR submitter: PAC = Pacific PNR = Prairie and Northern ONT = Ontario QUE = Quebec ATL = Atlantic NCR = Ottawa (HQ) VAR = Various LEGEND Feedback 2/2010 19 Make/ Model JASC Part Name Part No Part Condition SDR No. RGN ATR 42 320 2923 T PIECE MS21911D4 CHAFED 20090901008 PNR ATR 42 320 3234 LANDING GEAR SELECTOR STUCK 20090729002 ONT EC 135P2 6320 Z-ARIS DAMPER L633M2010108 LEAKING 20090402005 PNR AguStA A119 3210 CROSSTUBE FWD 109057004101 SHEARED IN HALF 20090512005 PAC AW119 MK II 3210 CROSSTUBE FWD 109057004101 SHEARED IN HALF 20090512004 PAC Air trACtor AT 802 2711 WIRE UNSERVICEABLE 20090501006 PAC AT 802 3246 WHEEL BEARING DESTROYED 20090806004 PAC AT 802A 2701 TRIGGER SWITCH 135L135R SHORT CIRCUITED 20091207003 PAC AT 802A 2752 STUD D186126 BROKEN 20090723009 PAC AT 802A 2821 INDICATOR PIN DETACHED 20090922005 PAC AT 802A 2841 FUEL IND FLAME-OUT 20090604002 PAC AT 802A 3210 ORING MS28775314 CUT 20090728004 PAC AT 802A 3220 NOSE GEAR SPRING 13A06633001 CRACKED 20091102003 ATL AT 802A 5512 R/H UPPER AUX FINLET CRACKED 20090902002 PAC AT 802A 5710 TUBE FRAME CLUSTER CRACKED 20091207002 PAC AT 802A 7280 FILTER EK905210 SEPARATED 20091207004 PAC AirBuS A310 304 2421 GENERATOR 729722CSN0561 CRACKED 20091109004 QUE A310 304 2497 WIRING DAMAGED 20090407015 QUE A310 304 3260 BRACKET SUB-ASSY GA595331 DAMAGED 20090505003 QUE A310 308 2910 HOSE 200595 LEAKING 20090522001 QUE A310 308 3150 CENTRAL WARNING SMOKE SMELL 20090514004 QUE A310 308 4930 DUCT PUMP A4933101500201 CRACKED 20091203003 QUE A319 112 1420 WIRE HARNESS E0266QF16 CHAFED 20090819001 QUE A319 114 2213 FLT AUGMENTATION COMPUTER B397BAM0513 FAULTY 20090421011 QUE A319 114 2720 RUDDER CONTROL SC47003 ACTUATOR BOLTS 20091202002 QUE A320 211 1000 PULLEY CUT 20090821004 QUE A320 211 2780 SLAT CONTROL FAILED 20091208003 QUE A320 211 2780 SLAT CONTROL FAILED 20091210004 QUE A320 211 3210 LANDING GEAR NOT LOCK UP 20091116006 QUE A320 211 3242 INBD WHEEL HALF 300796OPT2 FAILED 20090831002 QUE A320 211 3246 INBORD HUB 300796OPT1 MANGLED 20090602008 QUE A320 214 2330 CABLE ASSY RDAM68524 CONTAMINATED 20090512001 ONT A320 232 2612 PC BOARD (FIRE TEST) 350F51000 CORRODED AND WET 20090730001 ONT A330 243 2913 PRESSURE LINE TUBE AE71112112 CRACKED 20090929001 QUE A330 243 3242 STATOR PAD 215571 DESINTEGRATED 20091216008 QUE A330 243 8011 DUCT ASSY OF AIRSTARTER LJ41491 CRACKED 20090915002 QUE A330 342 2913 HYD PUMP 974800 LEAKING 20090709007 QUE A330 343 1497 WIRING MISWIRED 20090423004 QUE A330 343 2330 ENTERTAINMENT SYSTEM FAULTY 20090420003 QUE A330 343 2820 HARNESS ASSY F9298002800200 DAMAGED 20090504005 PNR A340 313 2560 AFT RELEASE PIN FAILED TO RELEASE 20090403001 QUE BAe - (rAytHeon) BAE 125 800A 3220 NOSE GEAR RETRACTION JACK AIR454041 LEAKING 20090909002 PAC HS 125 700A 5300 FUSELAGE DAMAGED 20090811002 ONT BAe - uK 3112 3230 RADIUS ROD ASSY 1862L FAULTY 20090609009 PNR 3112 3297 LG WIRING BROKEN 20091119005 PNR 3112 5544 FEELSPRING STRUT MOUNT CRACKED 20090618011 PNR 3112 8000 CONTACTOR AND GCU FAULTY 20090728010 PNR 3212 0 WINDOW WASH LIGHT 6645160S MELTED 20090728003 PNR 3212 3250 CABLE (LOWER) 137187E424 FRAYED 20090702011 PNR BeeCH 76 3245 TUBE 923150 DEFECTIVE 20090401016 ONT 100 3250 BARREL ASSY 50820042605 FAILED 20090401004 PNR 100 3260 LG WARNING FAULTY 20090909008 PAC 100 3497 DME 6221234012 SERVICEABLE 20090713002 PNR 200 2100 AIR CONDITIONING SEIZED 20090916007 PNR 200 2100 AIR CONDITIONING SIEZED 20090511003 PNR 200 2612 FIRE DETECTOR 302158 FAULTY 20090817002 QUE 200 2750 FLAP C FAILURE 20090618005 PNR 200 2750 FLAP RELAY SM50D7 FAILURE 20090618006 PNR 200 2823 SELECTOR VALVE STUCK 20090807003 PNR 200 2840 FUEL FLOW TRANSMITTER 903800097 FAILED 20090803002 PNR 200 2913 HYDRAULIC PUMP P3001 SPLINE WORN 20090507003 PNR 200 3213 TOR 1018100321 CRACKED 20090406004 ATL 200 3320 PANEL 10153005863 BURNT 20091027008 QUE 200 5210 DOOR FRAME 50430043865 CRACKED 20090619010 ONT 200 5210 DOOR FRAME 50430043865 CRACKED 20090624002 ONT 200 5310 INTERCOSTAL 1005303595 NEW 20091105003 PNR 200 5753 SKIN 10116000124 CHAFED 20090909004 PNR 200 7110 BRACKET/ANGLE 10191002221 IN SERVICE 20091006005 PNR 20 Feedback 2/2010 Make/ Model JASC Part Name Part No Part Condition SDR No. RGN 300 3231 LG DOOR FAULTY 20090611001 PNR 390 7310 FUEL LINE A91941 UNSERVICEABLE 20091002006 PNR 1900C 2100 AIR CONDITIONING 10238900611 LEAKING 20090507004 PNR 1900C 2432 BATT SYSTEM BURNT 20090708002 ATL 1900C 2435 GENERATOR FAILURE 20090505010 PNR 1900C 2750 FLAP C BROKEN 20090619002 PNR 1900C 2820 TUBE ASSY 3040637 CHAFED 20090511002 PNR 1900C 2820 TUBE 11492000023 WORN 20091023005 PAC 1900C 2913 POWER PACK MOTOR 481 FAILED 20090924009 PAC 1900C 3230 ELECTRIC POWERPACK MOTOR 571302 UNSERVICEABLE 20091103010 PAC 1900C 3234 LG SELECTOR FAULTY 20090508001 PNR 1900C 3251 STEERING INTERMITTANT 20090507002 PNR 1900C 5510 HORIZ/VERT DOUBLER CRACK (3 INCH) 20091118013 ATL 1900C 5700 WING CORRODED 20090519011 PAC 1900C 5751 REAR SPAR 11813000025 CORRODED 20091020005 PNR 1900C 5753 FLAPS BROKEN 20091215004 PNR 1900C 7200 ENGINE BLOWN OUT 20090921001 PNR 1900D 2497 C/B 7277210 INTERMITTENT 20090720001 ONT 1900D 2720 BRACKET L/H 1015240133 CRACKED BENT 20091104003 PAC 1900D 2750 FLAP FLEX SHAFT NO 3 1013800002 BROKEN/SHEARED 20091130003 ONT 1900D 3220 ACTUATOR 1123800222 CRACK 20091112002 ONT 1900D 3246 WHEEL BEARINGS CHANGED COLOR 20090504007 PAC 1900D 3340 LIGHTING CHAFED 20090423009 ONT 1900D 5711 SPAR CORRODED 20090504008 PAC 1900D 5753 AS ABOVE SHEARED 20090911006 PNR 1900D 5753 SHAFT ASSY 1013800002 UNSERVICEABLE 20090716010 PNR 3NM 5741 ATTACHED FITTING WELD CRACK 20091113008 PNR 3NM 7120 ENGINE MOUNT 18S9100 BROKEN 20091117004 ONT A100 3010 PEDESTAL TERMINAL BOARD MS2721226 DISCONNECTED 20090526004 PNR A100 3210 LANDING GEAR DAMAGED 20090401008 QUE A100 3233 NUT 508202085 FAULTY 20090420004 ONT A100 3260 LANDING GEAR FAULTY 20091223008 PNR A100 5753 CLIP 351153963 CRACKED 20090609003 ONT A100 7321 INTERCONNECT ROD 3010458 GOOD 20091223007 PNR B100 2100 FLOW 10138001317 VISUALLY GOOD 20091202018 PNR B100 2720 RESSORT & BOLVON 115524067AN12A BROKEN 20090611003 QUE B200 2100 BEARING 206SZZC SEIZED 20090901005 PNR B200 2100 AIR PLENUM 1015501472 SEPERATED 20090513002 PNR B200 2197 SWITCH 1015551531 BROKEN 20090730011 PNR B200 2710 AILERON CABLE NAS306351172 FRAYED 20090828001 PNR B200 2720 L/H RUDDER CONTROL CABLE 975240289 FRAYED 20091028004 PNR B200 2823 FIREWALL SHUT-OFF VALVE 1013890253 INTERMITTENT 20090526003 PNR B200 2840 HARNESS ASSY WET WING 10038006127 INTERMITTENT 20091102008 PNR B200 3210 LANDING GEAR DRIVE SHAFT 1018100213 CRACKED 20090413002 PNR B200 3210 LANDING GEAR COLLAPSED 20091031001 PNR B200 3210 LANDING GEAR INDICATION 20091208001 PNR B200 5210 SUPPORT 1014301781 CRACKED 20091204003 PNR B200 5310 VENTRAL FIN AND STRUCTURE 10144001885 DAMAGED 20090507010 PNR B200 5310 BULKHEAD 1014401091 CRACKED 20091204004 PNR B200 5311 FRAME CHAFED 20091110008 PNR B200 5313 FRAME - STA 207 10143002611 CRACKED 20090723007 PNR B200 5321 PANEL FLOOR 50440012553 CRACKED 20091204005 PNR B200 5412 BULKHEAD 1019800202 DETACHED FLANGE 20091204002 PNR B200 5712 RIB 50980002825 IN SERVICE 20090728011 PNR B200 5712 RIB 50980002825 IN SERVICE 20090728012 PNR B200 5753 FLAP ATTACH BRACKET 3516505031 WORN 20090714005 PNR B200 7110 BRACKET 101910049140 CRACKED 20091204007 PNR B200 7110 SKIN 1019100491112 CRACKED 20091204006 PNR B200 7200 ENGINE SMOKE 20090616009 PNR B200 7322 CONDITION LEVER CONTROL C 9938000131 UNSERVICEABLE 20090723006 PNR B200C 5300 SKIN CRACKED 20090526009 ONT B300 2100 BRACKET 11791006013 CRACKED 20090820011 PAC B300 2100 CABIN HEAT DUCT 30006761 DEFORMED 20090928005 ATL B300 2100 DUCT 30006741 DEFORMED 20090928006 ATL B300 2824 FLOAT SWITCH 1013890347 STUCK 20090429003 PAC B300 3210 AXLE PISTON ASSY 101810045601 ELONGATED HOLE 20091027001 ATL B300 3230 NOSE GEAR DOWNLOCK SWITCH 1003810061 FAILED 20090709002 PAC B300 5311 FRAME MOVING 20091118006 PNR B300 5510 HORIZ STAB NO DAMAGE 20091103003 ATL B300 5753 RIB 130116000011 CRACKED 20090415009 PNR B90 2730 ELEVATOR TRIM ACTUATOR 50524496 ON CONDITION 20090529004 PNR C90A 2730 PIN NAS427K26 SERVICEABLE 20090602009 PAC Feedback 2/2010 21 Make/ Model JASC Part Name Part No Part Condition SDR No. RGN C90A 3411 PITOT OPEN 20090904011 PAC C90A 7280 OIL CAP NOT SECURED 20090904010 PAC C90A 7921 TEMP CONTROL 723747 FAILED 20091214003 PNR E90 5311 SPLICE PLATES 9912005965 NEVER INSTALLED 20091020001 PNR E90 5520 CENTER ELEVATOR HINGE 5062000016 CRACKED 20090617003 PNR BeLL textron - CAn 206 5450 LWR SUPPORT ANGLE 206023131103 NEW 20091222008 PAC 206B 2562 E L T 4536604 FAULTY 20090922007 PNR 206B 2562 G SWITCH NEW 20090602001 QUE 206B 2700 LINEAR ACTUATOR 206062721113 FAULTY 20090730004 PNR 206B 2913 HYDRAULIC PUMP 206076022005 LEAKING 20090831004 PNR 206B 5302 PLATE 206032419001 UNSERVICEABLE 20091203007 PAC 206B 6230 SPERICAL BEARING 206010470101 UNSERVICEABLE 20090911005 PAC 206B 6230 SWASHPLATE WORN 20090528004 PNR 206B 6300 DRIVESHAFT 206040272101 OVERHEATED 20090915001 PNR 206B 6300 SEAL 206040272101 LEAKING 20090827006 ONT 206B 6500 DRIVESHAFT ASSY 206040330001 INCORRECT ASSY 20090525003 PNR 206B 6510 SEAL ASSY 206040272 BROKEN 20090417002 QUE 206B 6520 GEAR BOX 6894171 LEAKING 20090528003 PNR 206B 7120 ENGINE MOUNT LEG 206062102013 CRACKED 20090721003 PNR 206B 7323 GOVERNOR 23065121 STIFF 20090730005 PNR 206B 3 5312 BULKHEAD 206031200139 CRACKED 20090812007 ONT 206B 3 5510 R/H FITTING 206020121010 BROKEN 20090722008 PAC 206L 6220 FEATHERING BEARING 206011118001 SCRAP 20090518001 QUE 206L 6410 T/R BLADE 206016201131 GOOD 20090407012 ONT 206L 6410 TAIL ROTOR BLADE 206016201131 DE-LAMINATED 20091013003 ONT 206L 6700 COLLECTIVE ELBOW ASSY 206001154001 CRACKED 20090401009 PAC 206L 7230 CASE HALVES COMPRESSOR 23057142 UNSERVICEABLE 20090407013 ONT 206L 1 6320 CONTROL TUBE 2060011901 CRACKED 20090728016 PNR 206L 1 6320 MAIN DRIVESHAFT 206040015015 GREASE WASHED OUT 20090728015 PNR 206L 1 6320 SUN GEAR 2060405621 SPLINES WORN 20091217009 PAC 206L 3 5302 FITTING 206031403005P CRACKED 20091211005 PAC 206L 3 5510 SUPPORT UPPER L/H 206023119063 CRACKED 20090505002 PNR 206L 3 6210 M/R BLADE 206015011115 UNSERVICEABLE 20090706005 PNR 206L 4 2900 HYD POWER FAILED 20090923004 QUE 206L 4 6210 SPAR SPACER 206010106005 NEW 20090921004 QUE 206L 4 6420 NUT NAS1022A8 CRACKED 20091109001 ONT 407 5244 LATCH 90015032235 WORN 20091207006 PNR 407 5302 SUPPORT ANGLE 407023800129 CRACKED 20090605004 PAC 407 6210 M/R BLADE 407015001137 DELAMINATION 20090716007 PAC 407 6210 M/R BLADE 407015001137 DELAMINATION 20090716008 PAC 407 6220 SPRING 407310104105 SPRING FRACTURED 20091210001 ONT 407 6220 SPRING 407310104105 SPRING FRACTURED 20091210002 ONT 407 6230 BEARING 406310403101 MIGRATED 20090401001 QUE 407 6310 SEAL 209340265103 SEAL OUT 20091113004 QUE 407 6410 TAIL ROTOR BLADE 406016100119 SEPERATED 20090505006 ATL 407 6500 SLEEVE 206011732103 MOVED 20090608007 PAC 407 6510 AIRCOMM A/C PULLEY RING S3532EC5 OVERHEATED 20090406005 PAC 407 6710 SPRING 407001109103 BROKEN 20090928004 ATL 407 6720 PITCH TUBE 406012118101 DAMAGED 20090506007 QUE 407 7410 IGNITION EXCITOR BOX 2306130 FAULTY 20091002003 PNR 407 7910 ENGINE OIL TANK 206061505115 CRACKED 20090914011 PAC 412 6220 RACE 805045625 NEW 20090812006 PAC 412EP 7921 BLOWER 209062502101 CRACKED 20090917002 QUE 427 5530 BOLTS NAS660430 USED 20090901007 QUE BeLL textron - uSA 204B 5302 TAIL BOOM CRACKED 20090512011 PNR 205A 1 2435 STARTER/GENERATOR 204060200 SHEARED 20090619003 PNR 205A 1 2500 BUCKLE SL36L9SL36R9 CRACKED 20090826016 NCR 205A 1 6300 BOOT 2050401767 LEAKING 20091109002 PNR 205A 1 6500 FITTING 205031818001 CRACKED 20090702013 PNR 205A 1 6510 DRIVESHAFT COVER 205060922033 EXCELLENT 20090626008 PAC 205A 1 6510 FITTING 205031818001 CRACKED 20090424002 QUE 205A 1 7120 BOLT AN17412A BROKEN/CRACKED 20090818006 PAC 212 0 SCISSOR 212011407109 LOOSE BEARING 20090929004 PAC 212 1230 HYDRAULIC TUBE 212076433001 CRACKED 20090730008 PAC 212 2900 "T" FITTING AS1005W060606 CRACKED 20090511008 PAC 212 5302 FORMER LOWER & SUPPORT 212030124017 CRACKED 20091211007 ONT 212 5302 SUPPORT 205032817019 CRACK 20091211006 ONT 212 5302 TAILBOOM 212030128165B REMOVED 20091223005 QUE 212 5350 SKIN 212030099066 CRACKED 20090909003 PNR 212 5400 WASHER 204030913005 CRACKED 20090914002 ONT 212 5610 WINDSHIELD ASSY - R/H 212030464003 CRACKED 20090511007 PAC 212 6220 BARREL 204011143005 2 CRACKS 20091109006 PAC 212 6310 MAIN DRIVESHAFT 212040005103 BURNT 20090603006 PAC 212 6500 RETAINER PLATE 204040616001 WORN 20090727009 PAC 212 6520 SEAL 410082HAE LEAKING 20090511009 PAC 22 Feedback 2/2010 Make/ Model JASC Part Name Part No Part Condition SDR No. RGN 212 7200 VIGV ACTUATOR 118010601CV INCORRECT ASSY 20090914010 PAC 212 8300 BEARING #14 3120118101 SPALLING 20090702010 PAC 214B 1 6220 SPINDLE ASSY 214030606005 NEW FROM BELL 20090430003 PAC BeLLAnCA 14 19 5553 TAIL BRACE WIRE FORWARD BROKEN 20091019001 ONT Boeing 727 200 7532 DUCT 470962 RUPTURED 20090601004 ONT 727 223 5610 WINDOW 5893543130 CRACKED/BURNT 20090622005 ONT 727 225 2710 BEARING KP4A SIEZED 20091106006 ONT 727 225 5610 WINDSHIELD 5893543129 SHATTERED 20090611007 ONT 727 225 7830 SWITCH 62101 UNSERVICEABLE 20090827005 PNR 727 225A 5753 BOLT 69396421 DAMAGED 20090702003 ONT 727 227 5312 BOLT BACB30US10P37 SHEARED/CORROD 20091117005 PNR 727 233 3260 WIRE BROKEN 20090928001 ONT 727 243 5610 R2 WINDOW 57176244 UNSERVICEABLE 20090520004 PAC 727 247 2741 SWITCH 32EN144 USED 20091009003 PNR 727 247 5610 WINDOW CRACKING NOISE 20091224001 PNR 727 247 5753 FLAP HYDRAULIC MOTOR MS9391130ZE4C LEAKING 20090625004 PNR 727 260 2742 ACTUATOR CORRODED 20090526008 ONT 727 260 5610 WINDSHIELD 5893543129 ON CONDITION 20091022004 ONT 737 200 5430 ANGLE 654957323 BROKEN 20090618008 ONT 737 217 5610 WINDOW 58935733 CRACKED 20090514001 ONT 737 248C 5610 MIDDLE PANE SHATTERED 20090408004 ONT 737 275C 1000 SCREW BACB30NN4K11 BOTTOMED OUT 20091022001 PNR 737 700 2612 FAN CASE FIRE LOOP 325027302 CHAFED 20090929006 ONT 737 700 5300 EXOGRID CHAFFING 20091125005 ONT 737 700 5321 WET FLOOR AREA CORRODED 20091013002 ONT 737 7CT 2200 LOW RANG RADIO ALTIMETER 66500070101 FAULTY 20090821003 PNR 737 7CT 2710 ABSA AND ABSB BACC2A6B04398EG WORN 20091029002 PNR 737 7CT 3222 AXLE NLG SHEARED OFF 20090914006 PNR 737 7CT 5280 PUSHROD 162A31084 CRACKED 20090909007 PNR 737 800 2597 WIRING SHORTED 20090715003 QUE 737 81Q 5755 CABLE 580250403 BROKEN 20091217002 ATL 737 8AS 2330 CONNECTOR SJS816120 BURNT 20090708006 ATL 737 8AS 5430 PANEL 112N61012 CRACKED 20090601001 ATL 737 8BK 2810 ADAPTER PRESS FUEL SERVICE 2670054M2 LEAKING 20090717007 ONT 737 8HX 5610 SCUFF PLATE 141A48421 DAMAGED 20091202016 ONT 757 236 3416 STANDBY ALTIMETER LK359 OVERHAULED 20090421009 ONT 757 28A 2913 PRESSURE SWITCH 211C223327 ERATIVE 20091229003 ONT 757 2Y0 2497 WIRE W5100000520 SHORTED 20090622007 ONT 767 223 5610 WINDOW 141T480013 SHATTERED 20090618009 ONT 767 223 7500 SENSE LINE 332T12166 BROKEN 20090925003 ONT 767 333 3246 MAINWHEEL INNER BEARING M224749 FAILED 20091125001 QUE 767 333 7110 BRACKET CRACKED 20090702002 QUE 767 375 2100 ACM LUG FAULTY 20090818003 QUE 767 375 2100 AFT CARGO HEAT DUCT 214T640441 RUPTURED 20090702001 QUE 767 3Y0 3411 BRACKET BRACKET CHAFED 20090728006 QUE 777 233LR 1420 REGULATOR T0714R CARBON TRACES 20091007002 QUE 777 333ER 2100 SOFTWARE 3676GRS10400 MALFUNCTIONED 20091022003 QUE 777 333ER 2750 #8 TRANSMISSION 256W311010 FAILED 20090811001 QUE 777 333ER 2750 FLAP TRANSMISSION 256W311010 FAILURE 20090408003 QUE 777 333ER 7310 ENG FUEL FILTER HOUSING 18350 ARCHING DAMAGE 20091215003 QUE Boeing HeLiCopterS BV 107 II 7300 LIMIT SWITCH FAILED 20090911001 PAC BomBArDier BD 100 1A10 2131 CABIN PRESSURE CNTL 92175A030400 FAILURE 20090529005 QUE BD 100 1A10 2133 VALVE 81141A010302 FAULTY 20090626003 QUE BD 100 1A10 2140 ELECTRICAL HEAT MAT 343606 DISCOLORED 20090714007 QUE BD 100 1A10 2400 RSPC 980GC02Y06 BURNT/ARCING 20090728007 QUE BD 100 1A10 2900 EDP PRESSURE LINE ASSY 1005354233009 CRACKED 20090604008 QUE BD 100 1A10 2910 EDP PRESS TUBE (R/H) 1005354233009 LEAKING 20091002001 QUE BD 100 1A10 2913 ENGINE DRIVEN PUMP 5116003 OVERHEATED 20091119002 QUE BD 100 1A10 2913 QUICK DISCONNECT COUPLING AE99116J SEAL DAMAGED 20091104002 QUE BD 100 1A10 2916 HYDRAULIC RESERVOIR 33147500 LEAKING 20090710004 QUE BD 100 1A10 2923 PUMP 9558057 FAULTY 20090901006 QUE BD 100 1A10 3243 BRAKE CONTROL UNIT 14210451 VIBRATING 20091113007 QUE BD 100 1A10 5240 DOOR LATCH MISSING 20090825003 QUE BD 700 1A11 2450 AC POWER DIST 770705D FAILED 20090526001 QUE CL600 2B19 (RJ100) 1210 DRAIN FITTING 600627991 PLUGGED 20090710006 ATL CL600 2B19 (RJ100) 2150 DUCT 601R950687 LEAKING 20090405001 QUE CL600 2B19 (RJ100) 2200 AUTOPILOT FAULTY 20090428001 QUE CL600 2B19 (RJ100) 2420 WIRE XC3A8CORN BURNT 20090826017 ATL CL600 2B19 (RJ100) 2460 CONTACTOR D7GSZ CONTAMINATED 20090823001 QUE Feedback 2/2010 23 Make/ Model JASC Part Name Part No Part Condition SDR No. RGN CL600 2B19 (RJ100) 2460 RELAY UNDER VOLTAGE SENS VS643 FAILED 20090721001 ATL CL600 2B19 (RJ100) 2497 WIRING 756654A DAMAGED 20090512009 QUE CL600 2B19 (RJ100) 2520 PIN 1661038 CORRODED 20090816001 ATL CL600 2B19 (RJ100) 2710 AILERON C CONTAMINATED 20090423003 QUE CL600 2B19 (RJ100) 2710 BEARING 27295105 SEIZED 20090514005 ATL CL600 2B19 (RJ100) 2722 ACTUATOR ASSY 274273 INCORRECT ASSY 20091209001 NCR CL600 2B19 (RJ100) 2740 STABILIZER CONTROL STUCK 20090723001 QUE CL600 2B19 (RJ100) 2740 STABILIZER CONTROL FAULTY 20090906001 QUE CL600 2B19 (RJ100) 2740 STABILIZER CONTROL 83963 FAULTY 20090722001 ATL CL600 2B19 (RJ100) 2742 ACTUATOR 83963 FAULTY 20090724001 ATL CL600 2B19 (RJ100) 2750 BRAKE POSITION SENOR UNIT 855D1009 FAILED 20090729003 ATL CL600 2B19 (RJ100) 2750 SHAFT- FLEXABLE DRIVE 1104SD10040 BROKEN 20090618013 QUE CL600 2B19 (RJ100) 2750 UNIT SKEW DETECTOR 8004301 SERVICABLE 20090506010 PAC CL600 2B19 (RJ100) 2750 PDU 865D1007 FAILED 20091007003 ATL CL600 2B19 (RJ100) 2750 SKEW DETECTION UNIT 8004301 FAULTED 20091202004 ATL CL600 2B19 (RJ100) 2751 FPTU 601R930303 FAULTY 20090703005 QUE CL600 2B19 (RJ100) 2751 POSITION INDICATOR 855D10013 FAULTY 20090708008 ATL CL600 2B19 (RJ100) 2752 FLAP ACTUATOR 853D10019 INTERNAL DISCONN 20090502002 QUE CL600 2B19 (RJ100) 2752 FLAP ACTUATOR R/H #3 853D10024 FAULTY 20090405002 QUE CL600 2B19 (RJ100) 2752 FLAP ACTUATOR 85210023 FAILED 20091214006 ATL CL600 2B19 (RJ100) 2752 FLAP ACTUATOR 852D10023 FAILED 20091019007 ATL CL600 2B19 (RJ100) 2752 FLAP ACTUATOR 854D10023 FAILED 20091113009 ATL CL600 2B19 (RJ100) 2752 FLAP ACTUATOR 854D10024 JAMMED 20091206001 QUE CL600 2B19 (RJ100) 2760 FLIGHT SPOILER OUTBD PCU 270007 WRONG WARNING MESSAGE 20091107003 QUE CL600 2B19 (RJ100) 2840 FQGC 73664320 FAULTY 20090924002 QUE CL600 2B19 (RJ100) 3010 THERMAL SWITCH 601R593201 NEW 20090624004 ATL CL600 2B19 (RJ100) 3230 LANDING GEAR 16600101 FAULTY 20090619005 ATL CL600 2B19 (RJ100) 3230 LANDING GEAR 17051101 FAULTY 20090618014 QUE CL600 2B19 (RJ100) 3230 LANDING GEAR 4622 FAULTY 20090618015 QUE CL600 2B19 (RJ100) 3230 LANDING GEAR 2605890001 SEIZED 20090513006 ATL CL600 2B19 (RJ100) 3230 LANDING GEAR 750005000 WRONG WARNING MESSAGE 20091118002 QUE CL600 2B19 (RJ100) 3246 MAIN WHEEL 50105711 BROKEN 20090924001 QUE CL600 2B19 (RJ100) 3246 MAIN WHEEL ASSY 50105711 FLANGE CRACKED 20090629005 ATL CL600 2B19 (RJ100) 3250 NOSE GEAR STEERING ACT 16300106 UNSERVICEABLE 20091103004 ATL CL600 2B19 (RJ100) 3320 FLUORESCENT LIGHT FIXTURE BC10065003 SHORTED 20091218001 ATL CL600 2B19 (RJ100) 3397 PIN 1661038 CORRODED 20090813017 ATL CL600 2B19 (RJ100) 4900 APU 38004883 SEIZED 20090502004 QUE CL600 2B19 (RJ100) 4930 GUIDE VALVE 218423 MISSING 20090918003 ATL CL600 2B19 (RJ100) 4930 APU FUEL LINE 38834491 CHAFED 20090521004 ATL CL600 2B19 (RJ100) 4930 SHROUD AND FUEL FEED LINE C68C32 CORROSION/PUNCTU 20090616001 QUE CL600 2B19 (RJ100) 4960 CONTACTOR GENERATOR ZCDB9A023 OVERHEATED 20091118001 QUE CL600 2B19 (RJ100) 5210 ICE BREAKER CABLE 601R3181273 BROKEN 20090722009 ATL CL600 2B19 (RJ100) 5210 ICE BREAKER CABLE 601R3181273 FRAYED 20090722010 ATL CL600 2B19 (RJ100) 5210 INNER-HANDLE RETENTION- ME 6003804017 ON CONDITION 20090615003 ATL CL600 2B19 (RJ100) 5230 SURROUND FRAME RADIUS 601R250279 CRACKED 20091230001 ATL CL600 2B19 (RJ100) 5240 FITTING SERVICE DOOR 601R3872317 CRACKED 20091208005 ATL CL600 2B19 (RJ100) 5240 FITTING:SERVICE DOOR 601R3872317 CRACKED 20091208002 ATL CL600 2B19 (RJ100) 5344 FITTING 601R3807413 CRACKED 20091019002 ATL CL600 2B19 (RJ100) 5600 WINDSHIELD NP13932111 SHATTERED 20090407018 QUE CL600 2B19 (RJ100) 5610 SIDE WINDOW NP1393222 CRACKED 20090423002 QUE CL600 2B19 (RJ100) 5610 SIDE WINDOW NP1393226 SHATTERED 20090527004 QUE CL600 2B19 (RJ100) 5610 WINDOW CRACKED 20090407022 QUE CL600 2B19 (RJ100) 5610 WINDOW NP1393222 CRACKED 20090407019 QUE CL600 2B19 (RJ100) 5610 WINDOW SIDE (R/H) NP1393222 ELECTRICAL ARC 20091118004 QUE CL600 2B19 (RJ100) 5610 WINDOW SIDE (R/H) NP1393226 SHATTERED 20091118003 QUE CL600 2B19 (RJ100) 5610 WINDSHIELD NP13932113 CRACKED 20091107001 QUE CL600 2B19 (RJ100) 5610 WINDSHIELD (R/H) NP13932110 INNER PANE FAILED 20091206003 QUE CL600 2B19 (RJ100) 7110 LEFT UPPER ENGINE COWL 22850080801 LOST 20090525006 QUE CL600 2B19 (RJ100) 7200 FAN BLADE 6018T30P14 BENT 20090429001 ATL CL600 2B19 (RJ100) 7540 SENSING ELEMENT 356124310 DAMAGED 20090723003 QUE CL600 2B19 (RJ440) 3211 LG ATTACH 17307107 SWAPPED HYD LINE 20091228003 QUE CL600 2C10 (RJ700) 2460 LDCPC 900GC02Y01 FAILED AND BURNE 20090507001 QUE CL600 2C10 (RJ700) 2710 AILERON C CONTAMINATED 20090521002 QUE CL600 2C10 (RJ700) 2782 SLAT ACTUATOR 766385C FAILED 20091206002 QUE CL600 2C10 (RJ700) 3418 STALL WARNING C16258AA FAULTY 20090908003 QUE CL600 2C10 (RJ700) 5600 WINDSHIELD L/H NP1393215 CRACKED 20090407017 QUE CL600 2C10 (RJ700) 5610 SIDE WINDOW NP1393222 CRACKED 20090423001 QUE CL600 2C10 (RJ700) 5610 WINDOW NP13932112 CRACKED 20090407020 QUE CL600 2C10 (RJ700) 5610 WINDOW NP1393216 CRACKED 20090407021 QUE CL600 2C10 (RJ700) 5610 WINDSHIELD R/H 601R3303318 CRACK 20090413004 QUE CL600 2D15 (705) 2130 HINGE BA690951031 WORN OUT 20090623001 ATL CL600 2D15 (705) 3050 RADOME GC21905045 DELAMINATED 20091013006 ATL 24 Feedback 2/2010 Make/ Model JASC Part Name Part No Part Condition SDR No. RGN CL600 2D15 (705) 3242 FITTING QUICK DISCONNECT H155006191001 LOOSE 20090624003 ATL CL600 2D15 (705) 3610 PNEUMATIC SYSTEM GG67080301 EXPANSION BELOW 20090402004 ATL CL600 2D15 (705) 4990 OIL FILTER WE38817671 CRUSHED 20091102012 ATL CL600 2D24 (RJ900) 2131 CONTROLLER ACS GG69095026 FAULTY 20091107002 QUE CL600 2D24 (RJ900) 2200 AUTOFLIGHT SYSTEM INCORRECT 20090808002 QUE CL600 2D24 (RJ900) 2312 COMM SYSTEM 8221115001 FAILURE 20090602002 PNR CL600 2D24 (RJ900) 2360 STATIC DISCHARGE DAMAGED 20090501003 PNR CL600 2D24 (RJ900) 2400 CIRCUIT BREAKER MS220733 DAMAGED 20090502001 QUE CL600 2D24 (RJ900) 2530 GALLEY EQUIP BURNT 20090720005 QUE CL600 2D24 (RJ900) 2730 ELEVATOR CONTROL 510007 BROKEN 20091028012 QUE CL600 2D24 (RJ900) 3242 FTG HYD QUICK DISC H155006191001 INCORRECT ASSY 20090820010 QUE CL600 2D24 (RJ900) 3420 AHRU 6229336400 UNSERVICEABLE 20090723002 QUE CL600 2D24 (RJ900) 3500 CAPILARY LINE S70477 BROKEN 20090727006 PNR CL600 2D24 (RJ900) 5610 SIDE WINDOW NP13932211 CRACKED 20090808001 QUE CL600 2D24 (RJ900) 5610 WINDSHIELD NP13932113 CRACKED 20090624005 QUE CL600 2D24 (RJ900) 5610 WINDSHIELD NP13932114 CRACKED 20091111001 QUE CL600 2D24 (RJ900) 5755 PCU 5120011 JAMMED 20091002007 QUE CL600 2D24 (RJ900) 7200 ENGINE CF348C5 DAMAGED 20090606003 QUE CAnADAir CL215 1A10 2900 HYD PRESSURE LINE AE2460701H0170 CRACK 20090505007 QUE CL215 1A10 2913 PUMP 66WAL300 LEAKING 20090811003 PAC CL215 1A10 3242 BRAKE HOUSING 2604141 CRACKED 20091215005 PNR CL215 1A10 5240 PISTON 33130131 CRACKED 20091215001 PNR CL215 1A10 5330 FUSELAGE SKIN 21530027116 CRACKED 20091215007 PNR CL215 1A10 5711 FR 21510024808 CORRODED 20090402002 QUE CL215 1A10 7421 SPARK PLUG USED 20090527001 QUE CL215 6B11(CL215T) 5240 UPLOCK ACTUATOR 215750098 CRACK 20091106007 QUE CL215 6B11(CL215T) 7603 POWER LEVER RODEND 87620097025 LOOSE 20091105005 QUE CL215 6B11(CL415) 1497 WIRING OVERHEATED 20090505004 QUE CL215 6B11(CL415) 2810 FUEL CELL 21564002 LEAKING 20090910008 ONT CL215 6B11(CL415) 2820 FUEL PUMP HEATER T FITTIN B313007D4 INCORRECT ASSY 20091106005 QUE CL215 6B11(CL415) 3210 LOWER MEMBER 2158750162 CRACKED 20090901003 QUE CL215 6B11(CL415) 3233 NOSE GEAR ACTUATOR 15030016 FAULTY 20090812010 QUE CL215 6B11(CL415) 5244 WATER DOOR #3 215T3350617 CORRODED 20090609002 QUE CL215 6B11(CL415) 5310 FUSELAGE HULL CRACKED 20090421010 ONT CL215 6B11(CL415) 5620 R/H GLAZING WINDOW 215330176 LOST 20090615007 QUE CL600 2A12(601) 2932 CANNON PLUG SHORTED 20090414001 NCR CL600 2A12(601) 7700 SIGNAL CONTROL UNIT 601639039 UNSERVICEABLE 20090831001 NCR CL600 2B16(601 3A) 2913 MOTOR 9008D152 FAULTY 20090622006 QUE CL600 2B16(601 3A) 5320 FUSELAGE CRACKED 20090623003 QUE CL600 2B16(604) 2140 HEATER 307402 OVERHEATED 20090728002 QUE CL600 2B16(604) 2460 TERMINAL SH5PA & SH6PA JB17 BRULE 20090614001 QUE CL600 2B16(604) 2612 ELEMENT HT SENSING 24410457 CHAFED 20090731005 PAC CL600 2B16(604) 3100 RECORDING SYSTEM WRONG WARNING MESSAGE 20091201004 PNR CL600 2B16(604) 3234 SOLENOID 601R751451 OPEN CIRCUIT 20091202015 ATL CL600 2B16(604) 3320 NEON LIGHT AL1235T360 MELTED 20090401011 QUE CL600 2B16(604) 4900 BEARING FAILED 20090716001 QUE CL600 2B16(604) 7110 COWLING LOST 20090901004 QUE CL600 2B16(604) 7110 COWLING JAMMED 20091120002 QUE CL600 2B16(604) 7200 ENGINE WRONG WARNING MESSAGE 20091201001 QUE CL600 2B16(604) 7603 LEVER 1603730003 STIFF 20091218003 PNR CL600 2B16(604) 7603 SPRING CLIP 22850583801 WORN PIP HOLES 20091105001 ONT CeSSnA 150F 1000 FLOOR SCREW S1021Z810 SERVICEABLE 20090417001 PAC 150L 5412 BULKHEAD BENT 20090708001 ONT 150M 0 NOT REPORTED FAILURE 20090409003 ONT 150M 3245 TUBE TIRE 302246401 DEFECTIVE 20090401015 ONT 150M 3411 PITOT MELTED 20090421008 ONT 150M 5240 CHANNEL 41253330412 CRACKED 20091223006 QUE 150M 5347 STIFFNER 4102362 CRACKED 20090406007 ONT 152 1420 ELECTRICAL CONTACTOR S24752 OPEN 20091019004 PAC 152 2434 ALTERNATOR FAILED 20090708009 PAC 152 3220 NOSE GEAR FORK 4425037 UNSERVICEABLE 20091009001 PAC 152 5510 BRACKET 4320049 CRACKED 20090415006 PAC 152 5510 BRACKET 4320049 CRACKED 20090415007 PAC 152 5510 R/H REAR FIN BRAKET 4310093 GOOD 20091209005 QUE 152 5711 CHANNEL SPAR RIGHT HAND 4224056 CRACKED 20091026001 PNR 152 7414 MAGNETO 4381 RUNNING ROUGH 20091005007 ONT 172E 2701 YOKE 5117821 CORRODED 20090813006 QUE 172H 5540 RUDDER BRACKET 53101812 CRACKED 20090512007 PNR 172K 7430 IGNITION SWITCH C2925010105 WORN 20090710002 PAC 172M 3220 NOSE GEAR FORK 543043498 CRACKED 20091117002 ONT 172M 5412 BULKHEAD BUCKLED 20091021014 PNR Feedback 2/2010 25 Make/ Model JASC Part Name Part No Part Condition SDR No. RGN 172N 2436 VOLTAGE REGULATOR VR500010 FAILED 20091021010 PNR 172N 2820 FUEL VENT LINE VENTING OUT 20091005012 PNR 172N 3411 ALTERNATE STATIC VALVE 201314213 LEAKING 20091214005 PNR 172N 5520 BRACKET ASSY 5320061 LOOSE 20090618002 ONT 172N 7414 MAGNETO 4371 USED 20091110002 PNR 172N 8011 STARTER PRESTOLITEMHB4 BURNT 20091209006 QUE 172N 8011 STARTER 14924LS FAILED 20091102002 PNR 172P 2434 ALTERNATOR FAILED 20090915008 PAC 172P 2721 RUDDER CONTROL CRACKED 20091021005 PNR 172R 3340 SWITCH W31X100010 UNSERVICEABLE 20091103005 PNR 172RG 3210 LANDING GEARBODY ACTUATOR 12810016 HOLE IN CUSTING 20091019005 ONT 172RG 7800 EXHAUST SHOCK MOUNT 125025510 BROKEN 20091116001 PNR 172S 2434 ALTERNATOR FAILED 20090923003 PNR 172S 2710 AILERON CNTL BROKEN 20090708003 ONT 172S 2710 FAIRLEAD 52264712 WORN 20090902003 PNR 172S 3240 L/H BRAKE LINE CHAFFED LEAKING 20091020002 PAC 172S 3242 BRAKE LINE 500118127 WORN 20090908008 PNR 172S 3242 BRAKE LINE 500118126 PIN HOLE 20090908009 PNR 172S 3243 PISTON 98820125 BROKEN 20091102009 ONT 172S 8011 STARTER BROKEN 20090826006 PNR 172S 8011 STARTER BROKEN 20090618004 PNR 180J 2720 FORWARD RUDDER CABLE ASSY 510105173 FRAYED 20091103009 PAC 182A 5753 FWD FLAP RETURN CABLE 51010521 WORN/FRAYED 20090424004 PAC 182J 3210 LOWER OLEO FITTING 7436061 CRACKED 20090622003 ONT 182N 7111 RIGHT HAND SIDE COWL FLAP 752609201 DETACHED 20090520001 QUE 182Q 5300 SKIN LOWER FWD 07133343L/H CORRODED 20090902001 ONT 207A 5510 STABILIZER FR 12320131 CRACKED 20090522003 PNR 208 3246 FITTING 8A02700003 CORRODED 20091211011 PAC 208 5522 MASS BALANCE 2634014-1 CORRODED 20090924010 PAC 208B 2710 AILERON C FAULTY PART 20090615009 ONT 208B 2750 SUPPORT BRACKET 26111441 USED 20091207005 PNR 208B 3246 WHEEL ASSY 40179 FLAT TIRE 20090409001 ATL 208B 3246 WHEEL ASSY 16211800 CRACKED 20091002005 PAC 208B 5531 WEB 040 2024 26310217 FRETTED 20091022005 PNR 208B 7310 FLOW DIVIDER FAULTY 20091206006 ATL 210L 3220 CABLE ASSY RETR STEP 12115041 BROKEN 20090929003 PNR 210R 3233 LANDING GEAR MOTOR 98811411 OVER HEATED 20090430001 ONT 337G 3240 BRAKE WORN 20090712001 ONT 401A 3210 ADJUSTING SCREW 84113 BROKEN 20090710007 PNR 401B 8120 TURBOCHARGER BROKEN 20090807004 PNR 402 3210 DOWNLOCK SWITCH S20884 USED 20090616011 QUE 402C 3340 LIGHTING GEAR STRIPPED 20090513004 PNR 414 5730 WING SKIN CRACKED 20091116007 PNR 421C 3220 SKIN 52130409 CRACKED 20090728008 ONT 425 1000 NVT MS178263 MISSING 20090826004 NCR 425 2210 CLIP-TURNBUCKLE MS212561 MISSING 20090826005 NCR 425 2720 GUARD PIN NAS427K11 BROKEN 20090826003 NCR 425 2730 BRACKET ELV HINGE OTBD 58341309 CRACKED 20091021008 PNR 425 5330 PLATE 595105223 RUSTED AND PITTE 20091021007 PNR 425 5753 SKIN 512205393 CHAFED 20091021009 PNR 525 2731 ELEVATOR TRIM TAB C2TE43ATAB DISPLACED 20090617002 PNR 525 3010 HYDRAULIC ASSY 63170161 CRACKED-OFF 20091209004 ATL 525B 2915 HYDRAULIC PRESSURE SWITCH 99123734 INTERMITTENT 20091015005 PNR 550 2100 SPACER DEBONDED 20091015001 ONT 550 2730 ELEV TRIM CABLE 6565007108 WORN 20090825001 ONT 550 2731 R/H TAILCONE SKIN 651201030 WORN 20090821008 ONT 550 3220 NOSE GEAR UPLOCK LOOSE 20090609005 PNR 550 3220 WELDED NUT PLATE BRAKET CRACKED 20091211001 ONT 550 3220 WELDED NUT PLATE BRAKET CRACKED 20091211002 ONT 550 5347 LINK 5514501111 CRACKED 20091015002 ONT 680 3320 DOWNWASH LIGHT CLE23602 BURNT 20090807010 PNR 750 2100 AIR CONDITIONING FOREIGN OBJECT 20091128001 ONT A185F 7600 THROTTLE PLATE JAMMING 625601 FOREIGN OBJECT 20091005002 ONT R182 3310 TRANSISTOR 2N3055 BURNT 20090512010 QUE S550 2100 MOTOR BURNT 20090921005 PNR T206H 2421 AC ALTERNATOR FAULTY 20091216004 ONT T206H 2730 CABLES ICA8PR6 FRAYED 20090430004 ATL T206H 5240 SPLIT PIN NAS561P46 NEW 20090505009 ONT T210K 2750 FLAP FOLLOWUP CABLE 98600581 SHATTERED 20090826018 PAC T310P 3220 LANDING GEAR STUCK 20091124006 PNR TU206G 7314 FUEL PUMP ANEROID 6467683AR FAILED 20090707002 PNR U206 2710 SCREW AN5158R6 MISSING 20090402003 ONT 26 Feedback 2/2010 Make/ Model JASC Part Name Part No Part Condition SDR No. RGN U206E 2730 LOWER ELEVATOR CABLE 1260505129 FRAYED 20090707009 ONT U206E 5751 AILERON HINGE 12205317 CRACKED 20090707007 ONT U206E 5751 AILLERON HINGE OB 122005217 CRACKED 20090707008 ONT U206F 2434 ALTERNATOR FAILED 20090818002 PNR U206F 2730 ELEVATOR TRIM BROKEN SHAFT 20091202010 ONT U206F 3210 CENTERING LOCK 12436292 FAILED 20090707010 PNR U206F 3220 LANDING GEAR BENT 20090806010 PNR U206F 3246 BOLTS NAS14643NAS145 BENT 20090806008 PNR U206F 5730 SPAR BLOCK/SPAR PLATE 12221093 ORIGINAL 20091203006 PNR U206G 2421 ALTERNATOR DOFF10300BR FAILED 20090620001 PNR U206G 3213 FITTING 12116011 CRACKED 20090407008 PNR ConAir FIRECAT 2900 4 RIGID TUBING CHAFED 20090616004 PAC FIRECAT 3230 STRIKER UP LOCK SWITCH STICKY 20090603003 PAC FIRECAT 3233 DOOR 89H10547 INCORRECT ASSY 20090806014 PAC FIRECAT 3233 GEAR DOOR ACTUATOR 89H10527 LEAKING 20090723008 PAC FIRECAT 3242 BRAKE 147515 DAMAGED 20090608005 PAC FIRECAT 7300 PULLEY STRIPPED 20090723010 PAC FIRECAT 7600 CABLE SERVICEABLE 20090911002 PAC ConVAir - CAn 340 2434 AC GENERATOR 976J2525 FAULTY 20090622015 PAC 340 2750 FLAP C 20772 FAULTY 20090617008 PAC 340 2910 HYDRAULIC SYSTEM FAILED 20090824002 PAC 340 3020 DE-ICE SYSTEM DELAMINATED 20090720006 PAC 340 3260 SWITCH BZ7RQ67T UNSERVICEABLE 20090428003 PAC 340 7230 COMPRESSOR 6828400 DAMAGED 20091118005 QUE 440 2720 PIN CONSOLIDATEDVAL SHEARED 20090506013 PAC 440 3234 LANDING GEAR LEVER 3408500004 STICKY 20090623002 QUE 440 7210 REDUCTION GEAR FAILED 20090928002 QUE CurtiSS wrigHt C46D 2731 ELEVATOR CONTROL 201305756 CRACKED 20090722007 PNR C46D 7922 THERMOSTATIC VALVE LEAKING 20091027002 PNR DASSAuLt FALCON 20F5 3240 VALVE-RELAY EMERGENCY A11124654 LEAKING 20090819002 ONT FALCON 2000EX 2823 ACTUATOR D97D006071 FAILURE 20091103008 PNR DeHAViLLAnD - CAn DHC 2 MKI 1220 OIL CAP C2P383 LOOSE 20090625001 QUE DHC 2 MKI 2000 TORQUE TUBE C2UT473 CORRODED 20090817003 PAC DHC 2 MKI 2720 RUDDER CABLE ASEMBLY C2CF741AND FRAYED 20090402008 PAC DHC 2 MKI 2720 RUDDER C FRAYED 20090601006 ONT DHC 2 MKI 2720 RUDDER C FRAYED 20090601007 ONT DHC 2 MKI 2720 RUDDER C FRAYED 20090601008 ONT DHC 2 MKI 2730 ELEVATOR CABLE ASSY C2CF813A FRAYED 20090402009 PAC DHC 2 MKI 2730 ELEVATOR CABLE ASSY C2CF815A FRAYED 20090402010 PAC DHC 2 MKI 2810 FUEL COCK ELBOW C2P1107 CRACKED 20091009004 PAC DHC 2 MKI 2810 SUMP OUTLET PIPE NOPARTNUMBER CORRODED 20091015004 PNR DHC 2 MKI 2910 HOSE MILH6000 WORN 20090917003 QUE DHC 2 MKI 5311 BIRD CAGE C2FS3203A CRACKED 20090622004 ATL DHC 2 MKI 5520 TOR QUETUBE CORRODED 20090416006 PNR DHC 2 MKI 5551 BRACKET-FT TAILPLANE P/U C2TP159A CRACKED 20090407010 PAC DHC 2 MKI 5753 FLAP BRACKET L/H CENTER C2W143 CORRODED 20091229004 PAC DHC 2 MKIII 2701 CONTROL COLUMN LOWER C2CF33951 CRACKED 20091118010 ONT DHC 2 MKIII 3246 FITTING AFT WIRE PULL VALTBS12441 BROKEN 20090702012 NCR DHC 2 MKIII 3246 FITTING AFT WIRE PULL VALTBS12441 BROKEN 20090813016 NCR DHC 2 MKIII 5510 STAB ATTACH FITTING C2TP187A CRACKED 20090615004 PNR DHC 2 MKIII 5530 FWD STAB ATTACH FITTING CT2TF10291 CORRODED LEV 2 20091204011 PNR DHC 2 MKIII 5532 FUSELAGE FRAME C2FS705706 CRACKED 20090422002 PNR DHC 3 2701 CONTROL COLUMN SECTION C3CF48 CRACKED 20090421014 PAC DHC 3 2730 ACTUATOR SCREW C3CF2913 BINDING 20091021002 PNR DHC 3 2750 BELLCRANK ASSY FLAP C3CF4011 CRACKED 20091125002 QUE DHC 3 5342 BOLT NAS14729 CRACKED 20090910003 ONT DHC 3 5541 SPAR C3TF82 CRACKED 20090910002 ONT DHC 3 5544 BRACKET C3FS16911 CORRODED 20090606002 PNR DHC 3 5730 WING SKIN CORRUGATED 20091223001 QUE DHC 3 5753 FLAP CRACKED 20091201005 PAC DHC 3 7532 VALVE NOISY 20090707003 ONT DHC 3 8550 OIL FILTER 305925801 UNGLUED 20091223002 ONT DHC 3T 1000 BOLT HAS0004316 INCORRECT PART 20090424008 NCR DHC 3T 1000 BOLT NAS14729 NOT DAMAGED 20091027011 PAC DHC 3T 2400 CIRCUIT BREAKER MS265745 CRACKED 20091028001 QUE DHC 3T 3246 FRONT STRUT C3FU1086 CRACKED 20090424007 PAC DHC 3T 3246 FRONT STRUT C3UF1085 CRACKED 20090424006 PNR DHC 6 2751 FLAP POINTER ASSY C6JF12881 INCORRECT ASSY 20090902004 PNR DHC 6 3250 LEVER STEERING C6CFM123427 CRACKED 20090916003 PNR DHC 6 5540 RUDDER STOP ASSY TBDSCFS1837 RECALLED 20090817001 ONT Feedback 2/2010 27 Make/ Model JASC Part Name Part No Part Condition SDR No. RGN DHC 6 100 3246 BOLT AN620A BROKEN 20090703001 PNR DHC 6 100 7261 ENGINE PT6A20 SERVICEABLE 20090821002 ATL DHC 6 300 2421 CABLE C6NF10381 BURNT OFF 20090706006 ATL DHC 6 300 2497 GENERATOR RELAY CABLE C6NF10385 NEW 20090422001 PNR DHC 6 300 2730 CABLE ASSY ELEVATOR C6CF11491 BROKEN 20091030007 NCR DHC 6 300 2810 FUEL CELL C6SC10583 REPAIRED 20090619011 PNR DHC 6 300 2841 FUEL QUANTITY TRANSMITTER 39108703082 INSPECTED 20090610002 PNR DHC 6 300 3210 GEAR LEG ASSY R/H C6UM11108 INCORRECT PART 20090401006 PNR DHC 6 300 3210 MAIN LANDING GEAR C6UM11104 BROKEN 20090608006 NCR DHC 6 300 3220 PISTON TUBE 711419 DAMAGED 20090416002 PNR DHC 6 300 5730 UPPER SHROUD SKIN C6W100737 BROKEN 20091208008 NCR DHC 6 300 7300 DUST COVER C6PF105427 NEW 20090514002 PNR DHC 7 3250 SPIGOT STUD 161591 SHEARED 20090821007 NCR DHC 7 102 7170 TUBE ASSY 77900155003 INCORRECT ASSY 20091126002 ONT DHC 8 100 5610 WINDSHIELD 80260011 CRACKED 20090617004 QUE DHC 8 102 1000 BONDING JUMPER MS250837BBX USED/DAMAGED 20091123003 PNR DHC 8 102 1400 HARDWARE OVERHEATED 20091013007 ATL DHC 8 102 2400 ELECTRICAL WIRING CHAFED 20091118012 ATL DHC 8 102 2421 ALTERNATOR BURNT 20091221006 ATL DHC 8 102 2431 BATTERY OVERHEATED 20090821001 ATL DHC 8 102 2711 AILERON SPRING TAB HI L/H WORN 20090420001 ATL DHC 8 102 2720 FITTING ASSY - LOWER HING 85545002005 WORN 20091204010 PNR DHC 8 102 2910 TUBE ASSY 82970410119 CHAFED 20090929008 PNR DHC 8 102 2910 HOSE AND TUBE ASSY DSC3461 CHAFED 20090407009 QUE DHC 8 102 3210 ROLLER YCRS14 SEIZED 20090604007 ATL DHC 8 102 3230 LANDING GEAR - RELAY BASE CL12068161 UNGLUED 20091014002 QUE DHC 8 102 3231 LANDING GEAR DOOR DISCONNECTED 20091223011 ATL DHC 8 102 3232 GEAR DOOR ACTUATOR CAME LOOSE 20091223010 ATL DHC 8 102 3233 ACTUATOR LEAKING 20090615006 ATL DHC 8 102 3242 BRAKE FIRE 20090821005 PNR DHC 8 102 3411 PITOT PROBE PH11001DH POPPED 20090716003 ONT DHC 8 102 5210 FITTING 85321414111 CRACK 20091202001 ATL DHC 8 102 5210 FRAME ATTATCH ANGLE 85210025101102 CORRODED 20091023004 ATL DHC 8 102 5311 LOWER FRAME STA 240 5 CRACKED 20091104001 ONT DHC 8 102 5610 WINDSCREEN NP15790114 SHATTERED 20091014004 ONT DHC 8 102 5753 FASTENERS LOOSE 20091111002 ATL DHC 8 102 5755 SPOILER 85770013001 DELAMINATED 20090728001 ATL DHC 8 102 5755 SPOILER ACTUATOR A44700009 CRACKED 20090909005 ONT DHC 8 102 5755 CASING RUPTURED 20090406006 ATL DHC 8 102 5755 PULLEY 82742339001 SPLIT IN HALF 20091014001 ATL DHC 8 102 7220 UPPER FORWARD ENGINE COWL 87140002001 DENTED 20090807002 ATL DHC 8 106 1497 BRACKET 85321951101 ARCED DAMAGE 20091005005 PNR DHC 8 106 2000 EXCITER FAULTY 20091007005 PNR DHC 8 106 2497 WIRING BUNDLE CHAFED 20091021012 PAC DHC 8 106 2730 WASHER CSP19277 INCORRECT ASSY 20090805002 PNR DHC 8 106 2810 FUEL SHUT OFF VALVE LEAKING 20091022002 PNR DHC 8 106 2913 SEAL HYDRAULIC DRIVE 311859701 LEAKING 20090805005 PNR DHC 8 106 3241 ANTI SKID VALVE 39671 FAILED 20090927001 PNR DHC 8 106 5220 SEAL 85220255001 INCORRECT ASSY 20090806001 PNR DHC 8 202 2810 FUEL STORAGE FAULTY 20090529003 ONT DHC 8 202 5610 WINDSHIELD 8SC0043013 SHATTERED 20090714002 QUE DHC 8 300 2711 AILERON TRIM ACTUATOR LA11A2118 BROKEN ARM 20090908004 ONT DHC 8 300 2720 SWITCH 682175 SEIZED 20090416001 QUE DHC 8 300 2800 REFUEL DEFUEL ACCESS DOOR 85410618 BROKEN 20090903002 ONT DHC 8 300 2910 TUBE 829100100233 CRACKED 20090925001 QUE DHC 8 300 3260 LANDING GEAR CONTROL PANEL 860TS09Y00 FAULTY 20090625002 ONT DHC 8 300 5753 TORQUE TUBE ASSY 734386B SHEARED 20090929002 ONT DHC 8 301 2923 PUMP BURNT 20091130005 ATL DHC 8 311 1420 OVERHEAD LIGHT 7700301 SEVERELY BURNT 20091204008 QUE DHC 8 311 2910 HYDRAULIC PRESSURE LINE 82970010477 UNSERVICEABLE 20091223014 PAC DHC 8 311 3260 PHOTO SENSOR SD54434 FAILED 20090904001 ATL DHC 8 311 5610 BOLT COUNTERSUNK HEAD NAS71036 BROKEN 20090626006 ATL DHC 8 311 5610 WINDOW CAUGHT FIRE 20091021016 ATL DHC 8 311 5755 FITTING 85711566101 CRACKED 20091005008 PNR DHC 8 314 2710 AILERON I/P QUAD SUPPORT 85711569 CRACKED 20090717002 ONT DHC 8 314 2710 BEARING DAMAGED 20090616010 ONT DHC 8 400 1420 C 10962242 LOOSE 20090403008 QUE DHC 8 400 2421 AC GENERATOR 11522185 FAULTY 20090609001 QUE DHC 8 400 2421 AC GENERATOR 11522185 FAULTY 20090612001 QUE DHC 8 400 2497 WIRING CHAFED 20090928003 QUE DHC 8 400 2810 FUEL TANK PROBE 28069109 FAULTY 20091120001 ONT DHC 8 400 2913 ENG HYD PUMP 6617303 FAILED 20091013001 ONT DHC 8 400 2913 ENGINE DRIVEN HYDRA PUMP 6617303 SHAFT SHEARED 20091209010 ONT 28 Feedback 2/2010 Make/ Model JASC Part Name Part No Part Condition SDR No. RGN DHC 8 400 3210 SOLENOID SEQUENCE VALVE 483003 FAILED 20091209009 ONT DHC 8 400 3251 STEERING UNIT FAILED 20091020003 QUE DHC 8 400 7200 FADEC 8193007009 FAULTY 20090604003 QUE DHC 8 400 7700 FADEC 8193007009 REPLACED 20091223004 ONT DHC 8 400 7921 OIL COOLER EXIT DOOR ACT 800600M03 OVERHEATED 20090417003 ONT DHC 8 400 7922 OIL COOLER DOOR ACTUATOR 800600M02 FAULTY 20090610001 ONT DHC 8 402 2720 RUDDER C CHAFED 20090515004 ONT DHC 8 402 3210 SOLENOID SE 483026 FAULTY 20090604001 QUE DHC 8 402 3220 NLG RETRACT HYDRAULIC LIN 82910425003 PIN HOLE LEAK 20090528001 ONT DHC 8 402 3230 SOLENOID SEQUENCE VALVE 483003 MALFUNCTIONED 20091103001 ONT DHC 8 402 3411 PITOT STATIC PROBE C14135DA FAILED 20090421005 QUE DHC 8 402 5600 LEFT MAIN WINDSHIELD 80260007 SMOKE 20090917001 QUE DHC 8 402 5620 WINDSHIELD 80260008 SHATTERED 20090622001 ONT DHC 8 402 7500 SWITCH OVERTEMPERATURE 8209076 CROSS THREADED 20090928007 ONT DiAmonD - AS DA 40 2434 ALTERNATOR CB JUMPER WIRE DA431446003 DEFECTIVE 20090525005 ONT DA 40 3213 MAIN LANDING GEAR STRUT D41321311501 CORRODED 20091106003 ONT DA 40 8011 STARTER 149NLEC BROKEN 20090901002 PNR DA 40 F 3221 NOSE-LANDING GEAR STRUT D4132231000 CRACKED 20091102005 ONT DA 42 2600 FIRE DETECTOR FALSE INDICATION 20090619009 ONT DA 42 2810 FUEL TANK D40281700 CONTAMINATED 20091013010 ONT DA 42 3210 MLG BEARING HOUSING D6032176151 CRACKED 20090924006 ONT DA 42 3210 REAR BEARING HOUSING D6032176151 CRACKED 20090612003 ONT DA 42 3210 REAR BEARING HOUSING D6032176151 CRACKED 20090616007 ONT DA 42 3411 PITOT TUBE PST305 BENT 20090922006 PNR DA 42 5220 EMERGENCY HINGE RELEASE DA452000051 INSTALL ISSUE 20091119003 ONT DA 42 5280 R/H MLG DOOR AFT BRACKET D6052877400 CRACKED 20090924007 ONT DiAmonD - CAn DA 20 A1 2720 RUDDER CONTROL CABLES SF12579 WORN 20090928014 PAC DA 20 A1 2720 RUDDER CABLE SWAGED SLEEVE SLIPPED 20091007006 PAC DA 20 A1 2720 RUDDER CABLES 2027201300 NEW 20091127006 PAC DA 20 C1 2421 MOUNTING BRACKET 2224121400 BROKEN 20090709006 PNR DA 20 C1 2421 BRACKET ALTERNATOR 2224121400 CRACKED 20090528002 ONT DA 20 C1 2434 BRACKET ALTERNATOR 2224121400 CRACKED 20090714003 ONT DA 20 C1 2434 ALTERNATOR 887251 DAMAGED 20090408012 ONT DA 20 C1 2434 BRACKET ALTERNATOR 2224121400 CRACKED 20090604006 ONT DA 20 C1 3220 NOSE LANDING GEAR FORK 2032200800 CRACKED 20090825005 PNR DA 20 C1 5520 ELEVATOR MASS BALANCE 2255206002 HARDWARE MISSING 20091124004 ONT DA 20 C1 7310 FUEL DISTRIBUTION ENGINE QUIT 20090605010 ONT DA 20 C1 7600 INNER CABLE BROKEN 20090401003 ATL DA 20 C1 7600 INNER CABLE BROKEN 20091121002 ATL DA 20 C1 7602 ROD END HF3M WORN OUT 20090401002 ATL DA 20 C1 7602 INNER CABLE FRAYED 20091121001 ATL DA 20 C1 7602 ROD END HF3M WORN - SEPARATED 20091127004 ATL Dornier 328 100 2150 ENVIRONMENTAL CNTRL UNIT 5729C000003 REPAIRED 20090806012 PNR 328 100 2913 DC STANDBY HYD PUMP 4100849049 FAULTY 20090701002 NCR DougLAS DC9 2420 FILTER BOWL FRACTURED 20090722004 ONT DC10 30 5343 BOLT RA2230017 SHEARED 20090811006 PAC emBrAer ERJ 170 200 LR 2150 PACK NACA INLET BOOT 17055400401 WORN AND TORN 20091125008 PNR ERJ 170 200 LR 2780 SLAT CONTROL CRACKED 20091029004 PNR ERJ 170 200 SU 2710 L/H AILERON TOWER SHAFT 17009777407 STIFF 20090904009 QUE ERJ 170 200 SU 2710 AILERON CABLE 1703254100 UNALIGNED 20091021001 QUE ERJ 170 200 SU 2750 FLAP CONTROL FAILED 20091116004 QUE ERJ 170 200 SU 2780 SLAT CONTROL FAILED 20091210003 QUE ERJ 170 200 SU 2780 SLAT CONTROL FAILED 20091210005 QUE ERJ 170 200 SU 3610 WIRING HARNESS 170166603001 BURNT 20091021004 QUE ERJ 170 200 SU 5210 GIRT BAR FAULTY 20090908007 QUE ERJ 170 200 SU 5210 FLEXBALL CABLE 72CF10230 BROKEN 20090625005 QUE ERJ 170 200 SU 5280 NLG DOOR LINK - R/H AFT 17070760903 GOOD 20091214002 QUE ERJ 190 100 IGW 1210 REFUEL NOZZZLE 17009961403 BAFFLE ADRIFT 20091223013 QUE ERJ 190 100 IGW 2330 SVDU 179000201 UNSERVICEABLE 20090910009 QUE ERJ 190 100 IGW 2565 SLIDE 1040031 FAILED 20090504004 QUE ERJ 190 100 IGW 2612 FIRE DETECTION DISBONDED 20091116010 QUE ERJ 190 100 IGW 2612 STRUCTURE ADRIFT 20091028002 QUE ERJ 190 100 IGW 2612 STRUCTURE ADRIFT 20091028003 QUE ERJ 190 100 IGW 2750 FLAP CONTROL FAILURE WARNING 20090904003 QUE Feedback 2/2010 29 Make/ Model JASC Part Name Part No Part Condition SDR No. RGN ERJ 190 100 IGW 2750 FLAP CONTROL FAILED 20091202006 QUE ERJ 190 100 IGW 2750 FLAP CONTROL FAILED 20091202007 QUE ERJ 190 100 IGW 2750 FLAPS OPERATING RODS 1909238590 BENT 20091112001 QUE ERJ 190 100 IGW 2752 ACTUATOR FAILED 20091116005 QUE ERJ 190 100 IGW 2780 SLAT CONTROL FAILURE WARNING 20090904005 QUE ERJ 190 100 IGW 2780 SLAT CONTROL FAILED 20091126004 QUE ERJ 190 100 IGW 2780 SLAT CONTROL FAILED 20091210006 QUE ERJ 190 100 IGW 2782 SLAT ACTUATOR FAULTY 20090904004 QUE ERJ 190 100 IGW 2782 SLAT ACTUATOR 1703909 FAILED 20090813003 QUE ERJ 190 100 IGW 2782 SLAT ACTUATOR 1703909 FAILED 20090904002 QUE ERJ 190 100 IGW 2782 ACTUATOR FAILED 20091116003 QUE ERJ 190 100 IGW 2782 SLAT ACTUATOR FAILED 20091126003 QUE ERJ 190 100 IGW 2810 REFUEL DIFUSER 17009961403 DAMAGED 20091118011 QUE ERJ 190 100 IGW 3210 BEARING DUST SEAL MISSING 20090813005 QUE ERJ 190 100 IGW 3211 MLG RETRACT ACTUATOR PIN 2822A0000 CORRODED 20090921003 QUE ERJ 190 100 IGW 3211 RETRACT ACTUATOR ATT LUG 2822A000003 CORRODED 20090916002 QUE ERJ 190 100 IGW 3230 LANDING GEAR NO GREASE 20090813001 QUE ERJ 190 100 IGW 3230 LANDING GEAR FAULTY 20090813002 QUE ERJ 190 100 IGW 3230 LANDING GEAR WRONG WARNING MESSAGE 20091119001 QUE ERJ 190 100 IGW 3230 LANDING GEAR NOT EXTENDED 20091202005 QUE ERJ 190 100 IGW 3231 NLG DOOR LINK - R/H 17070760903 GOOD 20090610004 QUE ERJ 190 100 IGW 3242 BRAKE 90002340PR FAILED 20090428002 QUE ERJ 190 100 IGW 3246 WHEEL SEIZED 20090417007 QUE ERJ 190 100 IGW 3250 LANDING GEAR FAULT 20091202003 QUE ERJ 190 100 IGW 3251 STEERING UNIT FAIL MESH 20091116002 QUE ERJ 190 100 IGW 5320 SEAL REST 17067467001 CORRODED 20090813012 QUE ERJ 190 100 IGW 5544 COUNTER BALANCE WEIGHT CORRODED 20090629002 QUE ERJ 190 100 IGW 5554 BEARING DSRP8FS464 AXIAL PLAY 20090826001 QUE euroCopter Deut BK117 A 1D 6410 TAIL ROTOR BLADES (QTY 2) 117317411 USED/REMOVED 20091228002 PNR BK117 B 2D 6320 GEARBOX FAULTY 20091124001 PNR BK117 B 2D 6320 MAIN TRANSMISSION 1171200501 DEBRIS 20091124002 PNR BO105 S CDN BS 4 2911 HYDRAULIC TUBE 112145174 UNSERVICEABLE 20090407014 ONT BO105 S CDN BS 4 3340 LENS 1110001 SPALLED 20090421006 ONT BO105 S CDN BS 4 5302 TAILBOOM BO105 DISTORTED 20090508003 ONT BO105 S CDN BS 4 7310 FUEL CHECK VALVE 6895171 INCORRECT ASSY 20090706001 ONT euroCopter FrAnCe AS 332L1 6220 MR/H FLAPPING HINGE PIN SP 332A311401M FAILED 20090522005 PAC AS 355 5531 LOWER VERTICAL FIN 350A0855061601 CRACKED 20090402011 ONT AS 355 6220 YOKE 350A371162 CRACKED 20090908010 PAC AS 355 6320 MAST CHIP PLUG OVERHEATED 20090505008 ONT EC 120 B 0 BLANKING PLATE NPN INSTALLED 20090818004 PAC EC 120 B 2460 BATTERY/EPU SWITCH 045004A102A INTERMITTANT 20090417006 PAC EC 120 B 3340 RELAY LANDING LIGHT M610619017 INTERMITTANT 20090417005 PAC EC 120 B 5301 CAROUSEL SWITCH 83450001 NEW 20090702005 PNR EC 120 B 5301 CAROUSEL SWITCH 83450001 NEW 20090702007 PNR EC 120 B 6230 BOLT DHS4111012118 BROKEN 20090623007 PNR EC 120 B 6730 ELECTRO VALVE EVP310 FAILED 20090918001 PNR EC 120 B 6730 SERVO CONTROL SC50911 HARD OVER 20090812008 ONT EC 130 B4 3210 CLAMP ASNA0033097 FRACTURED 20090716004 ONT EC 130 B4 5301 CAROUSEL SWITCH 83450001 NEW 20090702006 PNR EC 130 B4 6297 ELEC CONNECTOR E0052R14B19SNF REPAIRED 20090716005 ONT FAirCHiLD SA227AC 0 GEAR HANDLE 2781014009 NOT SECURE 20090928008 ONT SA227AC 0 OB FLAP 2736000007 MISRIGGED 20090928012 ONT SA227AC 2100 COOLING TURBINE 20475546 NEW 20090506001 ONT SA227AC 2133 REGULATOR 38E852B REPLACED 20091211008 ONT SA227AC 2150 COOLING TURBINE 20475546 SEIZED 20090806006 ONT SA227AC 2400 BUS TIE SWITCH AN32302 INTERNALLY BURN 20091211010 ONT SA227AC 2400 CURRENT LIMITER ANL225 OVERHEATED 20091030006 PNR SA227AC 2900 HYD LINE 2781006019 CRACKED 20090828005 ONT SA227AC 2914 O RING MS287786 SPLIT 20090407006 ONT SA227AC 3200 LANDING GEAR LOW ACCUMULATOR 20091216009 ONT SA227AC 3230 GEAR CONTROL VALVE 246005 STICKY 20090806007 ONT SA227AC 3230 SWITCH 1EN516 INTERMITTENT 20091005003 ONT SA227AC 3250 ARMING VALVE 350501 NOT OPENING 20090519007 PNR SA227AC 5610 WINDSHIELD 2719442004 SHATTERED 20091113011 ONT SA227AC 5610 WINDSHIELD HEATED 2719442003 CRACKED 20091229001 PNR SA227AC 7200 TPE33111U ENGINE QUIT 20090512003 ONT SA227AC 7297 WIRE 19002716S BURNED 20090715001 ONT SA227AC 7500 BLEED AIR SYSTEM SMOKE 20090928009 ONT SA227AC 7730 AUTO IGNITION SWITCH 31057463 CRACKED 20090828003 ONT SA227CC 3233 LANDING GEAR 2751500001 WORN 20090522004 ONT 30 Feedback 2/2010 Make/ Model JASC Part Name Part No Part Condition SDR No. RGN SA227DC 2752 FLAP ACTUATOR 2736053003 LEAKING 20090629007 ONT SA227DC 2900 HYDRAULIC BYPAS LINE 27810322511 CHAFED 20091110011 PNR SA227DC 3222 LG STRUT 2752505 CRACKED 20090610003 PNR SA227DC 5610 HEATED WINDSHIELD - R/H 2719442002 CRACKED 20091216010 ONT SA227DC 7997 OIL TEMP BULB 52986 INACCURATE 20090928013 ONT FounD BrotHer FBA 2C1 3213 SHOCK ABSORBER TIE BOLT U320 USED 20090403011 ONT FBA 2C1 3246 FLOAT TIE WIRE LUG BROKEN 20090925004 ONT groB-werKe G 120A 2120 AIR DIST BURNING SMELL 20091103007 PAC G 120A 2421 RING TERMINAL 33466 ORIGINAL 20090902005 PAC G 120A 3260 LG WARNING FAULTY 20090922003 PAC G 120A 3430 LANDING AIDS BURNING SMELL 20090819005 PAC G 120A 3430 TAXI LIGHT HARNESS AWG20 OVERHEATED 20090819004 PNR G 120A 5730 WING DENTED 20091022006 PAC G 120A 7410 IGNITION/START SWITCH 103572101 SHORTED 20090909006 PAC guLFStreAm - iSrAeL GULFSTREAM 200 2600 FIRE DETECTOR LOOP UNSERVICEABLE 20090724004 ONT GULFSTREAM 200 2721 TRIM TAB ROD LOWER 4AS5820103501 UNSERVICEABLE 20091008005 ONT GULFSTREAM 200 2780 SLAT CONTROL FAILED 20090727004 ONT GULFSTREAM 200 2797 GROUND TERMINAL BLOCK BROKEN 20090601002 ONT GULFSTREAM 200 5610 TERMINAL END MS20659130 ARCED 20090715002 ONT GULFSTREAM G150 2752 MOTOR DC 5503D1003 SHORTED TO CASE 20090501002 PNR guLFStreAm - uSA 690C 3213 NLG RETRACT PISTON ED10145 CRACKED 20091215006 PNR HAwKer SiDDeLey-uK HS 748 2A 3260 BOLT 1000021303 BROKEN 20090605009 ONT HS 748 2A 7921 OIL COOLER RK35782A LEAKING 20090519009 QUE HugHeS 369D 6220 LOWER MR PITCH LINK BRG 369T795111 BEARING SEIZED 20090402007 PAC iSrAeLi inDuStrieS 1124 2900 HYDRAULIC POWER LEAKING 20090810001 ONT KAmoV KA32A11BC 6500 ROTOR FAULTY 20090408013 PAC LeArJet 31A 3230 UPLOCK SWITCH 1EN18 UNSERVICEABLE 20090519006 PAC 35A 2900 FITTING NUT AN622896D CRACKED 20091006001 NCR 35A 3234 HYDRAULIC SOLENOID VALVE 48C48641 FAULTY 20090918002 ONT 35A 5330 PLATE/SKIN CRACKED 20091123005 ONT 36A 2900 HOSE 2307006101 LOOSE 20091123001 ONT 45 2820 FUEL LINE 53A1101101 ORIGINAL 20090717003 ONT 45 2820 FUEL FEEDER LINE 244224151 LEAKING 20090514003 PAC 45 3010 H STAB FLEXIBLE L/H 66301000007007 CRACKED 20090414004 QUE 45 3010 H-STAB FLEXIBLE L/H 66301000007 FLEXIBLE PORTION 20090414002 QUE 45 3222 AXLE BEAM ASSY 2000203001 NEW 20090717005 ONT 45 3340 LIGHTING BURNT 20090714004 PAC 45 5330 SKIN CRACKED 20090918012 PNR 55 5720 DOOR ASSY 28260461 ORIGINAL 20091223003 ONT 60 3233 NOSE GEAR ACTUATOR LEAKING 20091202013 ONT 60 7830 INBOARD BRACKET 266000325 CRACKED 20090723005 QUE 60 7830 OUTBOARD BRACKET 266000325 CRACKED 20090723004 QUE LoCKHeeD 382G 1420 ELECTRICAL CONNECTORS FAULTY 20090727002 ONT 382G 3210 FS 517 BEAM R/H 331386961 CRACKED 20091007007 ONT 382G 7120 ENGINE MOUNT CORRODED 20090513003 ONT mitSuBiSHi - uSA MU 2B60 3231 GEAR DOOR ACTUATOR/ MOTOR AA5C INTERMITTENT 20091006002 ONT MU 2B60 5280 HINGE 030A35508 CRACKED 20090424003 ONT mooney M20E 7600 SWITCH V31 UNSERVICEABLE 20090813008 PNR morAVAn Z242L 2720 RUDDER CABLE Z14242260100 FRAYED 20090807001 ONT Z242L 2720 RUDDER CABLE Z14242260100 FRAYED 20090626002 ONT Z242L 2730 FWD ELEVATOR TRIM CABLE Z14244130000 FRAYED 20090508002 ONT Z242L 2731 AFT ELEVATOR TRIM CABLE Z4244120000 FRAYED 20090421003 ONT Z242L 2731 AFT ELEVATOR TRIM CABLE Z4244120000 INCORRECT ASSY 20090421004 ONT Z242L 2731 AFT ELEVATOR TRIM CABLE Z4244120000 INCORRECT ASSY 20090608004 ONT Z242L 2731 FWD ELEVATOR TRIM CABLE Z14244130000 FRAYED 20090605001 ONT Z242L 2750 FLAP CENTRE CABLE Z4243130000 FRAYED 20090626001 ONT Z242L 7120 ENGINE MOUNT L24263100000 CRACKED 20090430002 ONT Z242L 2720 RUDDER CABLE Z14242260100 FRAYED 20091001002 ONT Feedback 2/2010 31 Make/ Model JASC Part Name Part No Part Condition SDR No. RGN Z242L 2731 FWD ELEVATOR TRIM CABLE Z14244130000 FRAYED 20091001001 ONT Z242L 3240 BRAKE LINE Z4253100700 BROKEN 20091127001 ONT Z242L 3246 WHEEL RIM K2231007 CRACKED 20091028006 ONT Z242L 3250 STEER SPRING Z4242170001 BROKEN 20091112003 ONT Z242L 3250 STEERING CABLE E24242370000 FRAYED 20091210007 ONT piLAtuS - Sw PC 12 45 2100 TURBINE (COOLING) 1677D000002 SEIZED 20090423007 ONT PC 12 45 2133 SAFETY VALVE 1037842 FAULTY 20090415004 ONT PC 12 45 2210 AUTOPILOT FAULTY 20090415002 ONT PC 12 45 2711 ACTUATOR 978731813 SEPARATED 20090415005 ONT PC 12 45 2932 HYDRAULIC PRESSURE SWITCH 9738114304 LEAKING FLUID 20090526002 ONT PC 12 45 3020 INTAKE DEICE LIP 5302412140 CRACKED 20091118008 ONT PC 12 45 3040 WIRE H254A10H301A10 BURNT 20090618003 ONT PC 12 45 3060 S PACER MISSING 20090402001 ONT PC 12 45 3400 AHRU LCR-92 1242102011 INTERMITTENT 20091130002 ONT PC 12 45 3414 AIRSPEED INDICATOR 965121333 FAULTY 20090415003 ONT PC 12 45 5543 AFT TRIM STRIP 5554012038 CRACK 20091216007 ONT PC 12 45 5610 WINDOW 9598110111 CRACKE





